Windows Explorer, move to the working directory so you can drag and
drop conveniently
The minimized programs will show as buttons on the
task bar at the bottom of the screen. Click on the appropriate button
to access them. Remember to save your log, PHABSIM and spreadsheet
files often during the course of the analysis. Such a strategy will
prevent data loss due to the occasional inevitable mistake.
Laboratory 2. Building a PHABSIM Project
Objective
The objective of this laboratory is to cover the
use of PHABSIM for Windows to create a PHABSIM project file. PHABSIM
for Windows will be used to create an example project file and the
project will be reviewed for errors.
Data Files Used: Data.xls
Introduction
In typical PHABSIM applications, the user will likely
have a number of cross sections where the hydraulic characteristics
of the river channel have been measured at one or more discharges.
In this laboratory, we have provided data collected at four cross
sections from the Fryingpan River, where water surface elevations
and velocities have been measured at three calibration discharges.
All the hydraulic data necessary to create a complete PHABSIM project
file have been summarized in tabular form by cross section and provided
in Tables L1-1 to L1-4 at the end of this lab. Information about reach
lengths, Stage of Zero Flow (SZF), upstream weighting factors, reach
length, slope, best estimate of the discharge, and measured discharge
at each calibration flow is located at the top of each tabular summary.
The remaining data in the table lists the x?distance, bed elevation,
channel index, and observed velocities at each of the calibration
flows.
The laboratory illustrates use of \Edit\Cross
sections to enter the data for the four cross sections. Two complete
PHABSIM project data files containing these calibration data have
already been created (SAMPLE1.PRJ and SAMPLE2.PRJ) as example data
files. SAMPLE1.PRJ contains data entry only, while SAMPLE2.PRJ has
been run through the habitat simulation stage. Both projects are included
on the PHABSIM distribution disks. Proceed through the steps in order.
If you run out of time to enter all the data described below, you
can use SAMPLE1 to navigate the various menus and view diagnostic
plots. A separate set of worked laboratory exercise project files
is provided for each lab. The location of those files will vary depending
on the computer system used for class instruction.
Step 1. Create a New Data Set
Now that you understand the basic PHABSIM for Windows
navigation process from Lab 01, you are ready to open a new project
and enter data.
For ease of reference these instructions will use
the Project name MYLAB02.
\File\Open Project: Enter a project name in
the Project folder name box. Then type a description of the
project in the Project Description box. (The description is
limited to 256 characters.) Next use the Browse button to navigate
the Windows file tree to where you want the new folder to be stored.
PHABSIM for Windows will create a directory and a set of files with
the project name. For this lab, enter the new project name (i.e.,
MYLAB02) in the file name box, enter an appropriate description in
the project description box, then click Browse and navigate
to \IF310\Laboratories, and click OK. (See Figures L2-1, L2-1,
and L2-3.)

Figure L2-1. Opening a new project.

Figure L2-2. Assigning a folder location.
Figure L2-3. Entering project name and description.
An example of a project description might be:
"Fryingpan River 3 miles downstream from Reudi
Reservoir. High flow data collected May 10, 1999, mid flow data
collected July 10, 1999, and low flow data collected Aug. 23, 1999.
By name, name, and name."
You can revise the project description from the Edit
menu using \Edit\Project Data. This allows adding short notes
on the status of the analysis as the process progresses.
Step 2. Enter Project Hydraulic Data for Lab02
To build a project's data set, click the \Edit
menu item. You are presented with choices of Cross Sections,
Suitability Curves, and Discharges. You can enter and change
data for each of these categories by selecting the corresponding menu
item. However, you must begin with Edit\Cross Sections\Cross Section
Data and enter the cross section data for at least one transect
(cross section) prior to entering calibration data or coordinate data
as shown in Figure L2-4. The Edit\Cross Sections dialog contains three
tabs for Cross Section Data, Calibration Data, and Coordinate
Data. The Cross Section Data tab is displayed by default.
Figure L2-4. Preparing to enter cross section
data.
To create a new cross section, in the ..\Cross
Section Data tab, use the down arrow. A row of cells appears with
a cross section ID number of "-1.00". For each cross section,
enter the id for the cross section by typing the cross section ID
from Table L2-1 over the -1.00 entry. Move the highlight cursor to
the right with the right arrow and enter the reach length. Continue
moving to the right and enter the upstream weighting factor, the bend
weights for the Left Bank and Right Bank, the stage of zero flow (SZF),
Manning's n value (if known), Beta coefficient for MANSQ (if known),
and the energy slope. Values for Manning's n and beta can be left
unchanged for now. You would enter those values when using the WSP
or MANSQ models later in the analysis. Your data for the first transect
should now contain the following values.
|
ID
|
-
|
0.0
|
|
Length
|
-
|
0.0
|
|
Upstream WT
|
-
|
0.0
|
|
Left Wt
|
-
|
1.0
|
|
Right Wt
|
-
|
1.0
|
|
SZF
|
-
|
90.60
|
|
N
|
-
|
0.0
|
|
Beta
|
-
|
0.0
|
|
Slope
|
-
|
0.0040
|
Complete the cross section data table as shown in
Figure L2-5. Scroll right to include beta and slope values.
Figure L2-5. Entering cross section data.
Next, click on the cross section ID 0.00 line and
proceed to the Calibration Data tab (Fig. L2-6). Enter data
for either left and right bank water surface elevations, or
a single "user" selected water surface elevation, the user-determined
or "given" discharge for the study site, and the measured
discharge for the current transect. Enter these items for each calibration
discharge (matching each VEL set) for this study. Return to ..\Cross
Section tab to change to the next cross section ID.
Note that the best estimate discharge must be a unique
value (duplicates are not allowed). After you enter calibration data
and exit the calibration data tab, the table sorts in ascending order
on the Best Estimate Q values.

Figure L2-6. Entering calibration data.
Coordinate Data tab. Here you will find a
difference from historical PHABSIM data entry in that there are values
for X, Y, and Z. The inclusion of three dimensions is in anticipation
of the ability to import GIS or spatially referenced data in the future.
For now, enter the total distance upstream from the first transect
as Y. Thus, X represents distance across the transect from the head
pin, Y represents the distance upstream from the first transect (also
referred to as Stationing), and Z represents the vertical distance
above the datum selected for the study site. The program calculates
Y values and those cells have a gray background.
From the data in sheet xsec01 enter the x-distance
in column X, the distance upstream from the first transect in column
Y, and the elevation in column Z. Channel index and individual Manning's
n values for each cell are entered in the columns labeled CI and N.
Calibration velocity sets are entered in the Vel @discharge
columns. Enter the coordinate and velocity data from Table L2-1. The
coordinate data entry process is shown in Figure L2-7. When you have
finished, proceed to the ..\Cross Section Data tab, select
the next cross section and repeat the Calibration Data and Coordinate
Data entry steps.
Figure L2-7. Coordinate data entry.
These steps would normally be repeated for all transects
in the study. At that point, you have entered the basic hydraulic
data for the study site. In this lab, we will also learn how to input
coordinate data from a spreadsheet using Windows copy and paste functions
for the third and fourth cross sections in this project.
Entering Coordinate Data by Copy and Paste from a
Spreadsheet
PHABSIM for Windows allows entry of certain parts
of the project data using Windows copy and paste operations. The third
party data entry software has some quirks that must be accommodated
to enable the copy and paste features. The next steps demonstrate
how to paste coordinate data from a spreadsheet into PHABSIM for Windows.
Move to the ..\Calibration Data tab for cross
section 135. Enter (type) the calibration data contained in Table
L2-1. Now move to the ..\Coordinate Data tab for cross section
135.
Start your spreadsheet software and open the spreadsheet
named Mylab02.xls. Move to the worksheet labeled XSEC135. There you
will find a block of cells containing the X, Y, Z, channel index,
Manning's n, and calibration velocity data for this cross section.
Using the row index at the left, determine the number of rows of data
in the transect. Highlight this block of cells and execute the Windows
Copy command to copy those values into the Windows clipboard.
Return to PHABSIM for Windows using a mouse click
in that window.
Using the Insert or Down Arrow key,
insert the number of rows of data (not row numbers) found in the Coordinate
Data tab worksheet. (If you insert too many rows, right click
and select Remove Row as many times as needed. Then, using
the left mouse button, Drag the cursor from the lower left
(last X, last vel) corner of the worksheet to the upper left, being
sure to include the calibration velocity set columns. That entire
area should now be highlighted. Next, Right Click and select
Fill from the pop-up menu. The entire area will be filled with
0.00. Finally, move to the upper left corner of the coordinate data
entry area again. Right Click, and select Paste from
the pop-up menu. The highlighted coordinate data area will be filled
with the data from the spreadsheet. This process is shown in Figures
L2-8 through L2-10.

Figure L2-8. Opening and blocking coordinate
data tab rows.
Due to the nature of the data entry grid software,
calibration velocity cells that were blank in the spreadsheet now
have zeros. Delete those zeros using the Delete key so the
data set follows the convention that a blank velocity means the cell
was dry and a velocity of 0.0 means the cell had standing water. Compare
the PHABSIM for Windows data entry sheet with Mylab02.xls to ensure
all of the required velocity cells are changed to blank. Column Y
may change during this cut and paste operation, but it will revert
to the calculated value the next time you open this tab.
Figure L2-9. Filling the coordinate data table
with zeros.
Figure L2-10. Pasting coordinate data from
a spreadsheet.
Repeat these operations (Calibration and Coordinate
Data) for cross section 201.
Step 3. Enter Suitability Data for Lab02
Click \Edit\Suitability Curves and you are
presented with a dialog box where habitat suitability of use curve
(HSC) data can be entered for all species of interest for the study.
Begin by using ..\Suitability Curves\Edit\Add Curve and entering
the curve ID number and the species and life stage descriptions from
the HSC sheet in the Mylab02 spreadsheet in the boxes provided. Note
that curve ID numbers should be five or more digits to capture species
and life stage coding. Then click OK. A table for entry of
the Velocity curve information is displayed by default.
The same Insert key convention to create a
new line used with coordinate data entry applies. You may also copy
and paste HSC curves into PHABSIM for Windows using the conventions
described for coordinate data above. You must type the species, life
stage, and HSC number, but the coordinate data can be entered using
copy/paste operations.
Enter the HSC data for velocity by copy and paste
or by typing.
To switch to the Depth, Channel Index, or Temperature
HSC curves, click the appropriate button in the Curve Type box at
the upper right and enter the HSC data by paste or typing as above.
Repeat this process beginning with ..\Add Curve
for all HSC curve sets in the HSC sheet.
Enter Simulation Discharges for Lab01
This step may be performed now or after the hydraulic
models have been calibrated. To avoid excessive output during the
calibration process, the user would typically select to run the full
range of simulation discharges toward the end of the hydraulic model
calibration process. Those selections will be made in the WSL and
Velsim windows in later lab exercises. We will enter a small number
of additional discharges here to illustrate the process.
Select \Edit\Discharges to display the Simulation
Discharges window. The user-defined calibration best estimated discharges
(75.2, 139.0, and 250.0 cfs) are shaded in gray. They are automatically
entered in the Discharge column. Note that they are marked "cal"
in the Type column. Click on the first of these discharges and press
the Insert key. A new cell with a value of 0.00 will appear.
Enter a value of 15.0. Repeat this process with Insert (before the
calibration discharges) or the Down arrow (after one or more calibration
discharges) to enter the values of 60.0, 625.0, and 1250.0. Click
the Close button to end discharge data entry.
You have now finished the basic data entry process.
Save your project using \File\Save Project.
One more key data entry step remains, that of entering
Suitability-of-use criteria (SI curves). This topic will be covered
in Laboratory 7.
Step 4. Evaluate Diagnostic Plots
The quality of any modeling exercise begins with
correct data entry. PHABSIM for Windows contains several means of
viewing plots of the entered data for quality control. A longitudinal
plot of the observed water surface elevations can be obtained using
\Reports\Graphs\Longitudinal Profile and checking the Observed
WSL box. Selecting \Edit\Cross Sections\Coordinate Data and clicking
the graph button can view cross section geometry plots. The cross
section profile is displayed for the cross section currently selected
in \Edit\Cross Sections\Cross Section Data. To view different
cross sections, return to the ..\Cross Section Data tab and
select the desired cross section, then return to the ..\Coordinate
Data tab. Combined plots of velocities, water surface elevations
and bed geometry can be obtained using \Reports\Graphs\Bed Profile
with WSL\Velocities and checking the Observed WSL and Observed
Velocity boxes. You may wish to toggle on or off various calibration
discharges for clarity.
Step 5. Quality Assurance
As noted earlier, a longitudinal plot of the observed
water surface elevations can be obtained using \Reports\Graphs\Longitudinal
Profile and checking the Observed WSL box. Cross section geometry
plots can be obtained by selecting \Reports\Graphs\Bed Profile
with WSL\Velocities and checking the Observed WSL and Observed
Velocity boxes.
First, look at the longitudinal profile using \Reports\Graphs\Longitudinal
Profile, and then the cross section profiles for each transect
using \Reports\Graphs\Bed Profile with WSL\Velocities. In the
cross section profile plots, select the cross section and discharge
to be viewed in the tables to the left of the plot and click Refresh.
Examining the longitudinal profile of the water surface elevations
and thalweg depths in conjunction with the cross section profiles
for these data should indicate cross section 0.0 is a riffle (or channel
control) and that cross section 201 is in a pool. This is shown by
the increased depths at cross section 201 (see longitudinal profile)
as well as the more parabolic shape of the cross section profile at
station 201.
Note in Table L2-1, the velocity values at
verticals from 1.0 to 4.0 and vertical 44 have been left blank, since
these verticals were out of the water at each of the calibration discharges.
In general it is a good idea to examine the longitudinal
and cross section plots and note any areas that appear unusual. Are
there any characteristics of this data set that merit further attention?
Hint: look at the three velocity profiles for cross section
201. Look carefully at the shape of the velocity profiles and at the
stream margins. Do you see anything that does not make sense? Are
the longitudinal water surface profiles (look at longitudinal plot)
consistent? If there are any questions, you can refer to the original
field notes, consult with the crew members or look for other means
(assistance of a hydraulic engineer or hydrologist, for example) to
resolve inconsistencies.
Table L2-1. Data for cross section 0.0.
Cross Section 0
SZF 90.6
Upstream Weight Left Wt 0.5 Right Wt 0.5
Reach Length Left Dist 0.0 Right Dist 0.0
Slope 0.004
Manning's n 0.03
Beta 0.2
Calibration Data
LeftWSL RightWSL WSL BestEstQ Xsec Q
0.0 0.0 91.9 75.2 55.2
0.0 0.0 92.18 139 124
0.0 0.0 92.67 250 240
X Y Z Ci N VelSet1 VelSet2 VelSet3
2 0 94.8 6 0
4 0 94 6 0
6 0 93 6 0
8 0 92.7 6 0
10 0 91.9 6 0 0.00 0.00 0.90
12 0 91.3 6 0 0.10 1.30 1.50
14 0 91 6 0 0.50 1.50 2.40
16 0 91.1 6 0 0.50 1.70 1.80
18 0 91 6 0 0.2 1.40 2.00
20 0 91.1 6 0 0.00 0.30 1.00
22 0 91.3 5 0 0.00 0.30 0.80
24 0 91.7 5 0 0.00 0.30 0.50
26 0 92 6 0 0.00 0.50 1.30
28 0 91.8 6 0 0.00 0.90 0.60
30 0 91.8 6 0 0.00 1.30 1.80
32 0 92.1 6 0 0.00 1.00 1.20
34 0 91.8 6 0 0.50 1.80 2.30
36 0 91.5 6 0 0.60 1.60 2.20
38 0 91.5 6 0 0.60 1.60 2.60
40 0 91.5 6 0 0.90 1.30 2.00
42 0 91.5 6 0 0.60 1.40 2.40
44 0 91.5 6 0 1.10 1.10 2.00
46 0 91.3 6 0 0.60 1.40 2.80
48 0 91.4 6 0 0.60 1.80 2.40
50 0 91.2 6 0 1.00 2.30 2.60
52 0 91.3 6 0 1.20 2.50 2.90
54 0 91.4 6 0 1.60 2.40 3.20
56 0 91.4 6 0 1.50 2.60 2.80
58 0 91.2 6 0 1.70 2.60 3.10
60 0 91.2 6 0 1.90 1.80 3.40
62 0 91.1 6 0 1.90 2.60 3.20
64 0 91 6.3 0 1.60 2.30 3.10
66 0 91 6.3 0 1.70 2.40 2.90
68 0 91 6 0 1.50 2.90 3.20
70 0 90.8 6 0 2.00 2.20 3.00
72 0 90.7 6 0 1.50 2.50 3.00
74 0 90.8 6 0 1.90 2.50 3.10
76 0 90.6 6 0 2.00 2.60 3.00
78 0 90.8 6 0 1.70 2.30 2.80
80 0 90.9 6 0 1.50 2.00 2.00
82 0 90.9 6 0 1.50 1.70 0.60
83.5 0 92.64 6 0 1.00 1.70 1.10
86 0 92.8 6 0 0.00 0.80 0.00
88 0 94.8 6 0
Table L2-2. Data for cross section 60.0.
Cross Section 60
SZF 90.6
Upstream Weight Left Wt 0.5 Right Wt 0.5
Reach Length Left Dist 60.0 Right Dist 60.0
Slope 0.0032
Manning's n 0.03
Beta 0.2
Calibration Data
LeftWSL RightWSL WSL BestEstQ Xsec Q
0.0 0.0 92.08 75.2 61.4
0.0 0.0 92.42 139 129
0.0 0.0 92.95 250 265
X Y Z Ci N VelSet1 VelSet2 VelSet3
6 60 94.6 4 0
12.3 60 92.9 4 0
14 60 92.5 4 0 0.00
16 60 92.1 4 0 0.40 0.00 0.50
18 60 91.8 4 0 0.80 0.60 1.00
20 60 91.5 4 0 0.40 0.80 1.00
22 60 91.5 4 0 0.30 0.70 0.90
24 60 91.5 6 0 0.10 0.70 1.20
26 60 91.8 6 0 0.90 0.70 1.80
28 60 92 6 0 0.00 1.50 1.80
30 60 92.2 6 0 0.30 1.00 2.00
32 60 92.1 6 0 0.00 0.90 1.80
34 60 92 6 0 0.70 0.50 1.60
36 60 91.9 6 0 0.60 1.80 2.50
38 60 91.6 6 0 0.80 1.80 2.30
40 60 91.6 6 0 0.60 1.30 2.20
42 60 91.6 6 0 0.80 1.20 2.40
44 60 91.4 6 0 0.50 1.60 2.20
46 60 91.4 6 0 1.20 1.80 2.40
48 60 91.5 6 0 0.70 1.70 2.50
50 60 91.6 6 0 1.30 1.70 2.70
52 60 91.4 6 0 1.80 1.70 2.60
54 60 91.4 6 0 1.60 2.20 3.10
56 60 91.3 7 0 0.70 2.40 2.70
58 60 91.1 6 0 1.90 2.00 3.10
60 60 91 6 0 1.60 2.10 2.80
62 60 90.7 6 0 1.40 1.70 3.20
64 60 90.8 6 0 1.90 2.40 2.90
66 60 90.6 6 0 1.90 2.30 3.20
68 60 90.7 6 0 1.90 2.50 3.10
70 60 90.9 6 0 1.70 2.40 3.10
72 60 90.8 6 0 1.70 2.30 3.00
74 60 90.9 6 0 1.80 2.40 3.10
76 60 91.1 6 0 1.80 2.50 2.60
78 60 91.3 6 0 1.50 1.80 3.00
80 60 91 6 0 0.00 2.00 3.10
82 60 91.2 6 0 0.00 1.90 2.60
84 60 91.2 7 0 0.00 0.30 0.00
86 60 91.1 7 0 1.50 0.00 0.00
88 60 93 7 0 1.00 0.15 2.00
90 60 94.4 6 0 0.60
Table L2-3. Data for cross section 135.0.
Cross Section 135
SZF 90.6
Upstream Weight Left Wt 0.5 Right Wt 0.5
Reach Length Left Dist 75 Right Dist 75
Slope 0.023
Manning's n 0.03
Beta 0.2
Calibration Data
Left WSL Right WSL WSL BestEstQ Xsec Q
0.0 0.0 92.25 75.2 86.7
0.0 0.0 92.59 139 137
0.0 0.0 92.97 250 252
X Y Z Ci N VelSet1 VelSet2 VelSet3
6 135 94.3 4 0
10 135 93 4 0
12 135 92.8 2 0 0.00
14 135 92.5 3 0 0.00 0.00
16 135 92.4 3 0 0.40 0.00 0.00
18 135 92.3 3 0 0.80 0.50 0.60
20 135 92.1 6 0 0.40 0.70 0.00
22 135 91.6 6 0 0.20 0.90 1.70
24 135 91.5 6 0 0.60 1.30 1.30
26 135 91.5 6 0 1.10 0.70 1.70
28 135 91.1 6 0 1.30 1.60 2.60
30 135 91 6 0 0.90 1.70 1.80
32 135 91.1 6 0 1.30 1.20 2.70
34 135 90.8 6 0 1.70 1.40 2.60
36 135 91.1 6 0 1.70 2.30 2.90
38 135 90.8 6 0 1.60 1.30 3.20
40 135 90.6 6 0 2.10 2.30 3.30
42 135 90.5 6 0 1.80 3.00 3.00
44 135 90.7 6 0 1.50 1.80 3.40
46 135 90.7 6 0 1.90 2.20 3.30
48 135 90.8 6 0 1.60 2.70 2.80
50 135 90.7 6 0 2.00 2.30 3.00
52 135 90.9 6 0 1.60 2.00 2.90
54 135 91 6 0 1.90 2.30 3.10
56 135 90.9 6 0 1.60 2.00 2.50
58 135 91.2 6 0 1.60 1.40 2.90
60 135 91.3 6 0 1.60 2.00 2.70
62 135 91.3 6 0 1.30 1.70 2.20
64 135 91.4 6 0 1.30 1.50 2.20
66 135 91.6 6 0 1.00 1.40 2.40
68 135 91.6 6 0 1.10 0.80 2.00
70 135 91.6 6 0 0.30 0.80 2.10
72 135 91.6 6 0 0.00 0.60 0.90
74 135 92.3 6 0 1.80 0.30 0.00
Table L2-4. Data for cross section 201.0.
Cross Section 201
SZF 90.6
Upstream Weight Left Wt 0.5 Right Wt 0.5
Reach Length Left Dist 66 Right Dist 66
Slope 0.023
Manning's n 0.03
Beta 0.2
Calibration Data
LeftWSL RightWSL WSL BestEstQ Xsec Q
0.0 0.0 92.36 75.2 80.4
0.0 0.0 92.74 139 99
0.0 0.0 93.1 250 249
X Y Z Ci N VelSet1 VelSet2 VelSet3
4 201 93.9 6 0
6 201 93.1 6 0 0.00
8 201 92.8 6 0 0.00
10 201 92 6 0 0.00 0.00 0.70
12 201 91.6 6 0 0.30 0.00 1.00
14 201 91.5 6 0 0.40 0.30 1.20
16 201 91.2 6 0 0.50 0.40 1.40
18 201 91.2 6 0 0.50 0.50 2.20
20 201 91 6 0 0.60 0.60 2.50
22 201 90.8 6 0 0.70 0.80 2.50
24 201 90.5 6 0 0.80 0.90 2.80
26 201 90.3 6 0 0.90 1.50 2.80
28 201 90.2 6 0 1.10 1.50 2.90
30 201 90.1 6 0 1.20 1.90 3.10
32 201 89.9 6 0 1.50 2.30 3.40
34 201 89.8 6 0 1.60 2.40 3.30
36 201 89.9 6 0 1.90 1.80 3.30
38 201 89.9 6 0 1.90 1.60 3.00
40 201 90.3 6 0 1.50 1.00 2.70
42 201 90.4 6 0 1.30 0.90 2.40
44 201 90.7 6 0 1.80 0.70 2.00
46 201 91.3 6 0 1.40 0.70 1.80
48 201 91.6 6 0 1.10 0.40 1.80
50 201 91.9 6 0 0.60 0.20 1.30
52 201 92.3 6 0 0.40 0.00 1.40
54 201 92.7 6 0 1.60 0.00 0.80
56 201 92.7 6 0 1.60 0.00 0.80
58 201 93 6 0 1.30 1.70 0.00
60 201 93.1 6 0 1.30 1.50 0.00
61 201 93.1 6 0 1.00 1.40 0.00
66 201 94.1 7 0 1.10 0.80 2.00
68 201 96 7 0 0.30 0.80 2.10
Laboratory 3. Water Surface Modeling Using A
Stage-Discharge Approach
Objective
The objective of this laboratory is to demonstrate
modeling water surface elevations based on a stage-discharge regression
approach. The reader will be introduced to the use of the STGQ program
within PHABSIM for this purpose. The general theory of stage-discharge
modeling using a regression approach is covered in the manual in Chapter
3.
Program Used: STGQ
Project File Used: C:\My Documents\Phabsim\Laboratories\Lab3.phb
Introduction
The purpose of this laboratory is to introduce stage-discharge
regression modeling in PHABSIM using the STGQ model. Recall from the
lecture material that under most circumstances an investigator will
obtain measured water surface elevations at a specific cross section
at three or more flows, which is illustrated in Figure L3-1 for cross
section 0.0 for the Fryingpan River (see Laboratory 1 or access \Models\WSL\STGQ
Options\Stage Discharge Graph in the Lab3 project).

Figure L3-1. A stage-discharge relationship.
As discussed in Chapter 3, the relationship between
stage (i.e. water surface elevation) and discharge can often be represented
at a cross section in a channel by the following equation:
|
(WSL - SZF) = a Qb
|
(L3-1)
|
|
where:
|
Q = discharge
|
|
|
WSL = stage or water surface elevation
|
|
|
SZF = stage of zero flow
|
|
|
a = constant derived from measured values of
discharge and stage
|
|
|
b = coefficient derived from measured values
of discharge and stage
|
Note that the SZF is included in Equation L3-1 since
the stage-discharge relationship at a channel cross section is a function
of the SZF at that specific location as discussed in Chapter 3. The
SZF is used within the STGQ program and should be included whenever
using alternative stage-discharge regressions. Equation L3-1 can be
transformed to a linear relationship between stage and discharge by
taking the log10 of the equation, which yields:
|
log10 (WSL - SZF) = log10(a)
+ b * log10 (Q)
|
(L3-2)
|
Given at least three sets of measured stage-discharge
data at a cross section, a simple linear regression can then be performed
using Equation L3-2 to determine the constant and coefficient and
the resulting regression equation can be used to predict stage over
a desired range of discharges. The effectiveness of this modeling
approach for the simulation of water surface elevations is not only
a function of the observed data, but also the channel geometry and
relative difference in the slopes of the regression lines between
adjacent cross sections (see Chapter 3 of the manual).
In regression-based modeling, the primary modeling
choices involve the selection of the appropriate calibration discharges
(i.e., best estimate of discharge versus cross section specific [or
"local"] discharges), determination of an appropriate SZF,
and selection of the calibration water surface elevations. In this
laboratory, the best estimate of the discharge and average water surface
elevations will be used in the regressions. The SZF has also been
determined based on the thalweg bed elevations at each cross section
following the procedure outlined in Chapter 3 of the Manual.
Figure L3-2 contains the log of the water surface
elevations (minus SZF) versus the log of the discharges (best estimate)
for all four of the cross sections for the Fryingpan River. This figure
is provided to assist in an understanding of the laboratory data and
in the interpretation of the laboratory results.
Now proceed through the laboratory steps in the given
order.
Figure L3-2. Stage-discharge relationship for
four cross sections.
Step 1. Selection and Setup of STGQ Water Surface
Simulation Model
The complete project data set for the Fryingpan River
is supplied with the PHABSIM distribution disks and is named SAMPLE1.phb.
Begin by starting PHABSIM and opening the SAMPLE1
project. Select \Models\WSL. The Water Surface Elevation
Simulation window opens and the Output Options tab is displayed
by default. In this window the user can select which of the discharges
supplied earlier are to be used at the current stage of the simulation
process. For example, while calibrating the hydraulic models, it is
suggested to use only the calibration discharges. Thus, the check
boxes in the Use column should be toggled so only the "cal"
discharges are checked. When doing a final production run, all discharges
would be checked. In this lab, we are running a small number of discharges,
so leave this set at Use All.
In this window, you may also choose to overwrite
the ZOUT (results output) files. If you chose not to overwrite ZOUT,
successive runs of the models in PHABSIM append their results to ZOUT.
This can result in a very large file, but may be necessary when working
on a particularly difficult simulation. You may select Overwrite
ZOUT Filefor this lab by clicking on the box or the Overwrite
ZOUT File text so a check mark appears.
Next, click on the STGQ Options tab. Examine
the options (see Chapter 3) and make sure that you understand which
options are being used. In particular, note the Discharge (IOC Option
5) has been set to "Best Est Q" for all calibration sets
for all transects. This instructs STGQ to use the first "best-estimate"
discharge in the stage-discharge regressions. Setting the items in
the Discharge column to Xsec Q will use the discharge measured
at that cross section in the stage-discharge regression. This is not
necessarily equivalent to the best estimated discharge for the reach
at that calibration flow, but may provide a better fit to the observed
water surface elevation for individual cross sections under some conditions.
Also note that the project has seven simulation flows
ranging from 15.0 to 1250.0 cfs, which represent a range of discharges
both lower and higher than the three calibration, flows of 75.2, 139.0,
and 250.0 (see Laboratory 1). The higher and lower discharges allow
an evaluation of model performance over a simulated range of discharges
that is needed for the final habitat-discharge relation.
Step 2. Obtain the Calibration Water Surface Elevation
and Discharge Data
Select \Edit\Cross Sections\Calibration Data to
find the calibration data sets for the first cross section (i.e.,
cross section 0.0) and note the three calibration flows and their
observed water surface elevations.
The three calibration flows (best estimate of discharge as well as
the actual measured discharge at this cross section for each calibration
set) and the corresponding water surface elevations from the CAL lines
are:
|
Cross section 0.0
|
Best estimated Q
|
Measured Q
|
Water Surface Elevation
|
|
CAL1
|
75.2
|
55.2
|
91.90
|
|
CAL2
|
139.0
|
124.0
|
92.18
|
|
CAL3
|
250.0
|
240.0
|
92.67
|
Find and record the water surface elevations, discharges,
and SZF for all cross sections in Table L3-1 by first clicking on
the Cross Section Data tab, and on the next desired cross section,
then the Calibration Data tab. Once you have recorded the data in
Table L3-1, choose cancel and return to the Models\WSL\STGQ Options
tab.
|
Table L3-1. Calibration information
for the Fryingpan River.
|
|
Cross section
|
Best estimated Q
|
Measured Q
|
Water surface elevation
|
|
0.0 (SZF = 90.6)
|
75.2
|
55.2
|
91.90
|
|
|
139.0
|
124.0
|
92.18
|
|
|
250.0
|
240.0
|
92.67
|
|
60.0 (SZF = ____)
|
75.2
|
|
|
|
|
139.0
|
|
|
|
|
250.0
|
|
|
|
135.0 (SZF = ____)
|
75.2
|
|
|
|
|
139.0
|
|
|
|
|
250.0
|
|
|
|
201.0 (SZF = ____)
|
75.2
|
|
|
|
|
139.0
|
|
|
|
|
250.0
|
|
|
In this example, the best estimate of the discharge
was determined from an examination of the measured discharges at each
cross section. In some applications, the best estimate of the discharge
could have been derived from a gage within the reach or from the average
of a selected number of the measured transects where conditions for
obtaining good flow estimates was possible.
Step 3. Examination of the Stage-Discharge Relationships
The summary data in Table L3-1 was used to create
a plot of the observed longitudinal water surface elevations versus
discharge for the calibration data and a plot of the log of the discharge
versus the log of the (WSL-SZF) (see Figures L3-1 and L3-2).

Figure L3-3. Observed water surface profiles.
First, it should be apparent from the plot of the
longitudinal profile of the calibration data (Figure L3-3) that at
the high calibration flow, a flattening of the water surface elevation
is apparent at the middle two cross sections. This may be indicative
of a backwater effect at this discharge. Although backwater effects
can be pronounced more often at low flows due to riffle type habitats,
channel constrictions can produce this effect at higher discharges.
We do not know (since we did not collect this data) what is actually
occurring.
Examining the plot of the log-log relationship between
WSL-SZF and discharge shows that the observed data for cross sections
60 and 135 have almost identical WSL values at the high calibration
discharge (see Figure L3-2). This should indicate that using a regression
approach (i.e., stage-discharge with STGQ may be problematic at high
simulated discharges since the regression lines will likely >cross
over= each other. This will be explored in more detail in this laboratory.
Step 4. Running the Stage-Discharge Regression
Running the STGQ model to perform stage-discharge
regression modeling is basically an automated process once the appropriate
data have been entered and model options have been selected.
Select \Models\WSL\STGQ Options and ensure
that the SZF box is checked for each cal set for each transect (the
default). In rare instances removing the check mark can be used to
set the SZF used in the calculations to zero. You will not encounter
such a situation in this class. Click the Write Computational Details
check box so the program produces a file called ZOUT containing the
computational results. Once you have experience with PHABSIM, this
file can be omitted during the calibration process. It is often a
good idea to turn on this option when doing production runs in case
an "at the time" record is needed for documenting or defending
the study.
Next click the Assign Cal Sets button. Select
each transect using the dialog box in the upper left and ensure that
there is a check for each cal set for each applicable discharge. Selecting
All On means that the WSL for all discharges will be simulated
using all cal sets in the regression model. Under various circumstances
of data quality or channel configuration it may be desirable to use
only a portion of the available cal sets for a given discharge at
a particular cross section. Note: you may have more than three Cal
sets, but only certain ones may apply to specific cross sections.
That selection is made in the Assign Cal Sets table.
In PHABSIM for Windows it is possible to use different
water surface elevation models for different transects at different
discharges. Therefore, you must specify which model is being used
for each transect/discharge combination. Clicking the Method tab and
selecting a method from the list on the right and clicking the appropriate
position in the cross section discharge table accomplish this. For
this laboratory exercise, click STGQ and then click Set
All. This tells PHABSIM for Windows that the STGQ model will be
applied to all combinations.
Now you are ready to run the STGQ program. Simply
click the Run button at the bottom right. When the model has
finished running a "WSL Simulation Completed" message will
be displayed. To view the results, click OK and then click
the Results tab.
In the Results tab window you will see a table
of water surface elevations for each transect - discharge combination.
Plots of the water surface elevation results can be viewed by clicking
either the Cross Section or Longitudinal buttons at
the bottom.
Step 5. Evaluation of the Stage-Discharge Model
Results
At this point, we are interested in determining how
well the regression approach is working as a model for use in simulations
of water surface elevations. Figure L3-4 contains simulated water
surface profiles derived from the stage-discharge relations for the
four cross sections.
Figure L3-4. Water surface profiles simulated
with STGQ.
Click the Longitudinal button to view a plot
of the water surface profiles for each discharge as simulated by STGQ.
Remove checks from the Thalweg and Observed WSL boxes to arrive at
Figure L3-4. The top line in this graph (i.e., labeled SIM.(1250.0))
represents the predicted water surface elevation at a discharge of
1,250 cfs. The predicted water surface elevations at each cross section
are derived from each cross section's regression equation based on
the three sets of calibration data. At this discharge, water appears
to be flowing downhill from right to left in this figure. Note that
at 1,250 and 625 cfs, water is >flowing uphill= from cross section
135 to 60. These results are irrational from a physical standpoint
and indicate that the regression models are not appropriate at higher
discharges for this data set. In reviewing the simulation results
for 1250.0 cfs, it should be apparent that the >water flowing
uphill= between cross section 135 and 60 is >worse= than that observed
at 625 cfs. This suggests that the further you extrapolate above the
highest observed discharge (250 cfs) the more error in estimated water
surface elevation you will have.
At this point, we only know that somewhere between 250 and 625 cfs,
the stage-discharge regression approach >breaks down=. If we wanted
to better define where the model no longer works properly, we could
add additional QARD flows to our data set, such as 275, 300, 325,
etc., up to 625 and rerun the STGQ model. Examination of the output
would show the specific flow range at which water begins to 'run uphill'.
Based on our examination of the plotted longitudinal
profiles and the previous examination of the observed calibration
data we can more easily understand how these irrational results can
be generated by the regression modeling approach.
The STGQ program performs the regression analysis
at each cross section independently. Although the r2 for
the regressions at each cross section are > 0.99, the difference
in slope for each regression equation results in predicted water surface
elevations which cross at simulated discharges just above the
highest calibration flow. This should be expected given the observed
relationships between discharge and water surface elevations shown
in Figure L3-2, where the observed water surface elevations at cross
sections 60.0 and 135.0 are very close and tend to >converge= over
the range of observed discharges.
The modeling results would indicate that the stage-discharge
modeling approach may be valid at simulated discharges up to our highest
measured data (i.e., 250 cfs) but that an alternative modeling approach
for higher simulated flows will be needed. In Laboratory 4, the MANSQ
model will be used, while Laboratory 5 will employ the WSP model to
deal with this phenomena.
Step 6. Explore STGQ Regression Modeling Options
This section of the laboratory is optional and intended
to be completed at your convenience.
As indicated previously in the laboratory, the user
can select which of the cal set discharges to use in the regression
modeling with STGQ. In the previous laboratory steps, the stage-discharge
regressions were conducted using the best estimate of the discharge
by setting the Discharge (IOC 5) column to 'Best EST Q' for
all cross sections and cal sets. This forced STGQ to use the best
estimate of the discharge in the regression computations. In this
step of the laboratory, we will set these values to "Xsec Q"
so that the regressions are performed using the calculated discharges
at each cross section at each calibration flow.
If you are not in the \Models\WSL window,
move there now. Click the STGQ Options tab and click on the
first entry "Best EST Q". Next, click on the small wedge
arrow
to the right of the cell and then click "Xsec Q". Repeat
this for all cal sets for all transects.
To ensure the PHABSIM for Windows interface recognized the change,
go to the Methods tab and then click STGQ and click
any one of the transect - discharge cells to ensure the Apply
button becomes active. Then click the Apply button and view
results as before.
What you should find is that the 'error' values
in the regression equations have remained the same or increased and
that regression modeling of these data with discharges measured at
each cross section instead of a best estimate of discharge does not
eliminate the irrational results of simulated water surface elevations
at flows higher than our high flow calibration data set. Using the
computed discharges for each cross section can, and often will, result
in poorer linear relationships using Equation L3-2. This type of variability
between cross sections using computed discharges is not atypical when
field data has been collected in a variety of fisheries habitats which
are poor in terms of obtaining a >best estimate= of the discharge
for hydraulic modeling.
As a final wrap-up to this laboratory, go to the
STGQ tab and reset all of the discharges to Best EST Q. Then
go to the Methods tab, ensure that STGQ is marked and
click Select All. Click Run, go to results, and view
the longitudinal plot. Zoom on the calibration discharges (hold Shift
and drag a box with the mouse and release the mouse button) and print
the plot for later reference.
Laboratory 4. Water Surface Modeling Using the
MANSQ Model
Objective
The objective of this laboratory is to demonstrate
the technique of modeling water surface elevations based on using
Manning's equation (i.e., the MANSQ model). The general theory for
the MANSQ program is covered in the manual within Chapter 2.
Programs Used: MANSQ
Project Files Used: Lab4.phb
Introduction
The MANSQ model can be used to simulate the stage?discharge
relationship for individual cross sections. The model assumes that
flow variations caused by changes in channel configuration are negligible
(i.e., minimal backwater effects). The application of the MANSQ model
in pools can be problematic since pools are generally created by backwater
effects of a downstream hydraulic control. The MANSQ model assumes
that each cross section is independent of all other cross sections
during calibration and simulations. Therefore, the longitudinal profile
of the simulated water surface elevations should always be checked
to assess overall model performance.
At a computational level, the MANSQ model uses Manning's
equation in the form:
|

|
(L4-1)
|
which is simplified to:
The value of K is determined from a single measured
discharge-water surface elevation data set and the measured channel
geometry at a cross section. The program then uses additional calibration
data sets (i.e. discharges and water surface elevations) to solve
one of the following two equations selected by the user:
|

|
(L4-3)
|
|

|
(L4-4)
|
|
where:
|
subscript 'o' refers to calibration values
|
|
|
b is a coefficient
supplied by the user for each cross section
|
Calibration of the model is accomplished by selecting
an initial calibration discharge to compute Ko, and then
employing a trial and error procedure for selecting a value of
b that minimizes the error between observed and predicted water
surface elevations for the remaining calibration data sets. Typical
values of b range from 0.0 to 0.6 in most
channels and as noted in Chapter 2. The steps in this laboratory represent
a suggested order for MANSQ analysis.
Step 1. Obtain an Initial Estimate of b
Begin by initially setting that the b
value for each transect in \Edit\Cross Sections\Cross Section Data
to 0.2. This is an arbitrary default value derived from taking the
median value for a large number of study sites. Final
b values will be determined by observing the results of simulating
water surface elevations with MANSQ.
In this step, the CALCF4 program will be used to
obtain an initial estimate of b. Run the
CALCF4 program by clicking \Models\CALCF4. The results will
be automatically displayed to the screen. Scroll down the file and
locate the conveyance factor (CFAC) regression equation for cross
section 0.0. Alternatively, use the Notepad editor to search for "CFAC"
in the current ZOUTx file.
The exponent of the CFAC regression equation represents
an excellent initial estimate for b and
is -0.003 for cross section 0.0. Continue through the output listing
to locate and record the CFAC regression exponents at the three remaining
cross sections. Record these values in Table L4-1.
Note that the CFAC regression exponent at cross section
0.0 is negative. Under most circumstances, the use of negative b
values is not expected since this would imply that roughness would
be increasing with discharge. In typical applications of MANSQ, a
negative b would be rounded up to 0.0 for
use in the model.
|
Table L4-1. CFAC regression exponents
for each cross section.
|
|
Cross section
|
CFAC exponent
|
|
0.0
|
-0.003
|
|
60.0
|
|
|
139.0
|
|
|
201.0
|
|
Once the remaining CFAC exponents have been entered
in Table L4-1, exit Notepad if you have been using it to find the
CFAC exponents and return to \Models\WSL\MANSQ in PHABSIM for
Windows.
The MANSQ program requires a calibration flow and
water surface elevation at each cross section in addition to the initial
estimate of b. These data are derived from
the calibration data sets entered in \Edit\Cross Sections\Calibration
Data for each cross section. For this laboratory, the high flow
calibration data at each cross section will be used as our initial
calibration flow for MANSQ.
|
Table L4-2. Calibration discharges and
water surface elevations for the Fryingpan River from MANSQ
using 250 cfs (Cal Set 3) as the calibration discharge.
|
|
Calibration Q
|
Cross section 0
|
Cross section 60
|
Cross section 135
|
Cross section 201
|
|
75.2
|
91.90
|
92.08
|
92.25
|
92.36
|
|
139
|
92.18
|
92.42
|
92.59
|
92.74
|
|
250
|
92.67
|
95.95
|
92.97
|
93.10
|
NOTE: You may choose either the high, medium
or low flow calibration data sets (or any combination for specific
cross sections). However, selection of the calibration discharge should
be considered of the flow ranges most critical to the study. Remember,
MANSQ will 'return' the observed water surface elevation at the calibration
flow and the 'error' between predicted and observed water surface
elevations at the other calibration discharges will be a function
of the field data and selection of appropriate b's.
We will select b's to minimize the error
between observed and predicted WSL at each transect.
Step 2. Running the MANSQ Model and Evaluating
Results
Select the \Models\WSL\MANSQ tab and note
the options available in the MANSQ program and review the options
that have be set. For this laboratory exercise, the default options
will suffice. However, advanced users may wish to consider the alternative
ratios of flow conditions given in equations L4-3 and L4-4, and other
MANSQ options.
Next, click on the Methods tab and click MANSQ
followed by Set All. This assigns MANSQ as the model to be
applied to all cross sections at all discharges. Now click Run.
Since we have chosen the high calibration flow (i.e.,
250 cfs) MANSQ will always return the observed water surface elevations
for this flow at each cross section. We need to evaluate the predicted
water surface elevation at each cross section for the medium (139
cfs) and low (75.2) calibration flows.
The Results tab contains a table of predicted
water surface at each of the simulated discharges for each cross section.
Click the Print button to obtain a copy of this table for later
use. Click the Longitudinal button to view a plot of the longitudinal
profile for all discharges. Click the check boxes for Observed
WSL and Simulated WSL. Note the wild divergence of the
WSLs at transects 135 and 201. The steep water surface elevation at
high flows is unrealistic for a pool. In addition, the water surface
elevation at the lowest discharges runs uphill. Our initial b
values are not working too well.
Compare the predicted water surface elevations at
139 cfs and 75.2 cfs for each cross section against the observed water
surface elevations for these calibration flows. It is apparent that
an initial estimate of b of 0.2 results
in a prediction of the water surface elevations at cross sections
0 and 60 that are too low, while this same b
results in a prediction of water surface elevations at cross sections
135 and 201 which are too high at the high discharges and too low
at the low discharges.
This means that b coefficients
at all cross sections need to be adjusted in order to obtain better
agreement between observed and predicted water surface elevations.
Table L4-3. MANSQ calibration table.
X-Sec 0 Obs-WSL ß:0.20 ß:0.02 ß: ß: ß: ß: ß:0.00
250 cfs 92.67 92.43
139 cfs 92.18 92.15
75.2 cfs 91.90 91.90
X-Sec 0 Obs-WSL ß:0.20 ß:0.02 ß: ß: ß: ß: ß:0.00
250 cfs 92.95 92.68
139 cfs 92.42 92.35
75.2 cfs 92.08 92.08
X-Sec 0 Obs-WSL ß:0.20 ß:0.02 ß: ß: ß: ß: ß:0.32
250 cfs 92.97 93.12
139 cfs 92.59 92.66
75.2 cfs 92.25 92.25
X-Sec 0 Obs-WSL ß:0.20 ß:0.02 ß: ß: ß: ß: ß:0.51
250 cfs 93.1 93.68
139 cfs 92.74 92.99
75.2 cfs 92.36 91.36
Step 3. Trial and Error Calibration of MANSQ by
Adjusting b at Each Cross Section
You have now obtained an initial solution of the
water surface profile using MANSQ but some adjustment is needed. Return
to \Edit\Cross Sections and change the
b coefficient from 0.20 to 0.02. Make this same change to the
b value at cross sections 60 to 201. Note that these new estimates
of b have been entered in Table L4-3.
Click OK to exit Edit\Cross Sections and save the
file changes. Return to \Models\WSL\Methods, check that the
MANSQ method is selected, and click Set All again. When the
program has finished, click OK and Results as before.
Compare the Results table displayed on the screen to the one you printed
earlier. What happened to the predictions for the water surface elevations
when we increased or decreased b at the
cross sections?
You should find that increasing b
will result in predicted water surface elevations which increase for
discharges above the calibration discharge, while decreasing b
results in the predicted water surface elevations decreasing. The
opposite will be true below the calibration discharge.
Return to \Edit\Cross Sections and change
the b values for each cross section to
induce the needed change in WSL at each transect to match the calibration
discharges. Record these values in Table L4-3. Remember to use a b
value of 0.00 instead of negative values for any cross section. Save
these changes and re-run the MANSQ program and record the new predictions
for the water surface elevations at each cross section for the medium
and low calibration flows in Table L4-3. How close are the predictions
of water surface elevations?
Based on these results, make adjustments to the b
values as necessary. Your strategy should be to minimize the error
between predicted and observed WSLs at both the 139 cfs and 75.2 cfs
calibration flows for each cross section (you cannot get them both
to be exact) by selecting the 'best' b
for each cross section. Remember, MANSQ treats each cross section
independently, so if you get a particular cross section to work, you
no longer have to adjust the b value at
the cross section while continuing your calibration efforts at other
cross sections. You should make several trial runs during the lab
in your quest for the best fit; however, due to class time limitations,
the final calibration b values are provided
in Table L4-3.
Step 4. MANSQ Final Calibration Run and Hydraulic
Diagnostics
Up to this point we have focused on the calibration
discharges and have not dealt with the WSL for the other discharges
in the data set. The particular b values
entered at the far right in Table L4-3 generally result in a maximum
error between observed and predicted water surface elevations at the
calibration flows, which range between 0.00 and 0.06 feet. This magnitude
of difference is on par with the results obtained from the stage?discharge
regression approach covered in Laboratory 3. However, we still need
to check the effectiveness of the hydraulic simulations further by
looking at the longitudinal profile of the water surface elevations
at all simulated discharges.
View the longitudinal plot in \Models\WSL\Results
again. Expand to full screen using the Windows maximize button for
the graph window. It is useful to print this graph and label it MANSQ
final for later reference.
The thalweg depths for each cross section are displayed
as the bottom line with the x-axis indicating the distance between
each cross section moving in an upstream direction. The top line in
this graph represents the water surface elevation at a discharge of
1250 cfs. Using the key at the bottom of the plot, the other discharges
can be identified by their line and symbol combinations. To aid in
viewing simulated water surface profiles only, the Observed WSL
check box can be left blank (click to remove check).
The predicted water surface elevations at each cross
section are derived from the MANSQ model based on the calibrated b's.
At this discharge, water appears to be flowing downhill for some cross
sections and uphill for others.
Note that at the simulated discharge of 625 cfs,
water is 'flowing uphill' between cross sections 3 and 2. Although
excellent agreement can be obtained with MANSQ for the calibration
data, the simulated water surface elevations at discharges greater
than 250 cfs are irrational.
At this point, we know that somewhere between 250 and 625 cfs, the
MANSQ model 'breaks down' in a similar fashion to the results obtained
using the IFG4 model in Laboratory 3. The reason behind the production
of irrational results with MANSQ for this data is basically similar
to the reasons discussed in Laboratory 3 using IFG4. In MANSQ, the
b value represents the exponent in a power
law relationship (see Equations L4-3 and L4-4) that approximately
tracks the changes in Manning's n over a range of discharges. Therefore,
b acts as the 'slope' factor for the relationship
between water surface elevation and discharge. Since the measured
water surface elevations at cross sections 60.and 135 are very similar
at the high calibration flows (see Table L4-2), the 'best fit' relationship
derived from matching the water surface elevations at the two lower
calibration flows 'causes' the predicted water surface elevations
to 'cross over' at simulated discharges above 250 cfs.
At this point, an alternative modeling approach for
the simulation of discharges greater than our high flow calibration
(i.e., 250 cfs) should be considered. Given the nature of these data,
modeling options within MANSQ are not likely to improve the simulation
results (i.e., use of Equation L4-4 rather than Equation L4-3). Given
the results already examined in Laboratory 3 using IFG4, the WSP model
would be the next step and is examined in Laboratory 5.
Laboratory 5. Water Surface Modeling Using the
WSP Model
Objective
The objective of this laboratory is to demonstrate
the technique of modeling water surface elevations based on the step-back
water method as implemented in the WSP model. We will cover the steps
of finding an overall Manning's n value that is a "best fit"
for the study site, adjusting n values to capture localized roughness
differences at each transect, and specifying roughness modifiers to
accommodate the change in n value as a function of discharge. The
general theory for the WSP program is covered in the manual in Chapter
3.
Programs Used: WSP
Project File Used: Lab5.phb
Introduction
The WSP model is a water surface profile program
that is used to predict how the longitudinal profile of the water
surface elevation changes over a range of simulated discharges. The
initial objective in the calibration of the model is to use a trial-and-error
procedure to select Manning's n coefficients at each cross section,
which will replicate the longitudinal profile of the water surface
elevations at this single calibration flow. This requires that the
bed geometry elevations and water surface elevations have been measured
to a common benchmark or elevation datum (i.e., the cross sections
are 'dependent' and connected). We first attempt to find a global
value (or overall channel roughness value) for n that is applied at
each cross section to produce a "least error fit" of the
water surface elevation profile to the observed data for one discharge.
We then vary Manning's n for each cross section (within reasonable
limits) to achieve a reasonably close fit between observed and predicted
water surface elevations. Finally, we use a trial-and-error procedure
to select main channel and overbank roughness modifiers that produce
the best fit between observed and predicted water surface profiles
for all remaining calibration flows. The relationship between the
calibrated roughness modifiers and discharge is then used to develop
either a regression equation or a good linear approximation, from
which we can estimate the appropriate roughness modifiers for all
simulation discharges of interest.
WSP requires a starting water surface elevation or
energy slope as an initial condition. We have already found stage-discharge
relationships using a regression approach (i.e., STGQ) and by calibrating
MANSQ for the downstream cross section. To provide WSP with the needed
initial condition, the user selects the combination of starting conditions
based on using the water surface elevation derived from STGQ or MANSQ
in the \Models\WSL\Methods tab by clicking on ..\WSP\STGQ
supplies initial WSL or ..\WSP\MANSQ supplies initial WSL
or ..\WSP\User supplies initial WSL. The two combined WSP\XX
options take the starting water surface elevation from one of those
models and supplies it to WSP. The WSP\User option allows the user
to set this value manually. The ..\User supplies WSL (no model
run) option allows users to import WSL values for the entire study
area and discharge range from an outside source.
In this laboratory, we will select the high flow calibration data
as the starting point in the calibration of the WSP model. In particular,
we are interested in determining if this modeling approach can overcome
the problem with simulated water surface elevations at higher discharges
encountered when using a stage-discharge regression (i.e., STGQ in
Laboratory 3) or the MANSQ model (Laboratory 4). The laboratory also
provides a discussion of the implications of using a different initial
calibration flow and resulting impacts to simulated water surface
elevations. The given steps represent a suggested order for WSP analysis.
Step 1. Prepare Data and Select Options to Run
the WSP Program
We begin by setting the same initial Manning's n
roughness value for all cross sections. Start PHABSIM for Windows
and load Lab5.phb. Select \Models\WSL\WSP Options and note
that a Manning's n value of 0.030 has been entered for all cross sections.
WSP requires that the water surface elevations at
the down stream cross section for each discharge are supplied to the
model as boundary conditions. For discharges of 75.2, 139, and 250
cfs we know the actual observed water surface elevations at the down
stream most cross section (i.e., cross section 0.0). However, the
water surface elevations for the remaining four discharges are not
known. To resolve this issue, we use STGQ or MANSQ to obtain water
surface elevations for the downstream cross section. From Labs 2 and
3 we know that STGQ produces a slightly better fit between observed
and simulated water surface elevations at cross section 0. Thus, we
will use STGQ as the source of starting water surface elevations.
Move to \Models\WSL\Methods and first select
WSP (click the radio button) followed by Set All. This saves
clicking on each element of the table separately. Now select the
..\WSP\STGQ radio button and click in the cross section 0.0 row
for each discharge. (Be sure and scroll the table so all cross section
0.0 entries for all cross sections are filled with WSP-S. This sets
all initial conditions to use the WSL from STGQ and applies WSP to
all cross sections at all discharges.
We have the measured water surface elevations for
the three calibration discharges. Will they be different than those
predicted by STGQ? To ensure the best precision in calibrating WSP,
it is wise to use the known values as the initial conditions. For
the three calibration discharges, select ..\WSP\User supplies initial
WSL and click the cross section 0.0 entry for each discharge and
enter the starting WSL from the data. You have already entered this
data as part of the calibration data sets, but to allow for improved
estimates of the starting WSL, you must enter it here also.
In the \Models\WSL\WSP Options tab, there
is a table for entering roughness modifiers (RMODs) for each discharge.
The RMODs are used by WSP to adjust the Manning's n values derived
in the initial calibration of the longitudinal water surface profiles
to account for changes in roughness as a function of discharge. The
default value for the RMODs is '1', so initially there is no variation
in Manning's n with discharge. These values are modified by the user
as needed to obtain a reasonable fit between observed and simulated
water surface profiles.
For this exercise, we will use the high discharge
as our reference discharge. This is generally a good practice when
using WSP as calibration residual errors tend to compress (get smaller)
as one simulates downward using backwater type models. As trial values,
set the roughness modifiers for 139 cfs and 75.2 cfs to 1.1 and 1.2,
respectively. These are strictly trial values so you can start by
leaving them at 1.0 if you wish.
Step 2. Run the WSP Program and Determine the Initial Water Surface
Elevation Predictions
Click the Run button now to run the combined
STGQ (at cross section 0.0) and WSP (at all cross sections) model.
A message window will indicate when the WSL simulation is completed.
Click OK to clear this window.
Select the \Models\WSL\Results tab or \Reports
and click on the longitudinal plot option. Select Observed
and Simulated WSL followed by Refresh. Zoom on the three
calibration discharges by holding down the Shift key, moving the mouse
to the lower left corner of the region you wish to zoom, holding the
left mouse button and dragging to the upper right corner of the
zoom area. Then release the mouse button and the plot will zoom to
that area. Note that \Models\WSL\Results contains a table of
water surface elevation information for all cross sections and all
discharges. In this case, it has seven entries in each row corresponding
to the seven discharges we have directed the model to simulate. Note,
for example, that the predicted water surface elevation associated
with the 250 cfs calibration flow at cross section 201 is 92.936.
How do the simulated values compare with the observed
values? Note from the plot that at all three calibration discharges
the simulated water surface profile falls considerably below the observed
profile. An adjustment to Manning's n is needed. The table in the
\Models\WSL\Results tab can display the observed, simulated, and
difference in water surface elevation at the calibration flows by
clicking the Cal Comparison radio button. This is useful to
display numerical values for the differences seen in the plot.
Step 3. Calibrate WSP for the Longitudinal Water
Surface Profile at 250 cfs
For the calibration process it is useful to prepare
a table such as Table L5-1 to record successive iterations of the
Manning's n adjustment process. The first estimate of the water surface
elevation at cross section 60 at 250 cfs recorded in Table L5-1 shows
that the predicted WSL is low by 0.185 feet. The calibration strategy
will be first to change the Manning's n values at all cross sections
simultaneously to get the predicted water surface elevation at all
cross sections for our chosen discharge of 250 cfs to fit through
the observed values for all cross sections in a reasonable manner.
Generally, we would like the simulated values to fit the observed
values as closely as possible. We expect some values to be high and
some to be low at this stage. Go back to \Models\WSL\WSP Options
and raise the Manning's n to a new, higher value for all cross sections
(.045 is suggested). Remember, raising n increases roughness will
thus raise the simulated water surface profile.
Return to Models\WSL\WSP Options and make
sure the roughness modifier for a discharge of 250 cfs has a value
of 1.0. Then click the Run button to run the model. Repeat
this process of setting Manning's n, running the model, and viewing
results until you have achieved a satisfactory fit between the simulated
and observed water surface profile for the 250 cfs discharge.
Figure L5-1 shows the plot resulting from raising
Manning's n to 0.45 at all cross sections. Display this plot by clicking
the Longitudinal button in the ..\WSL\Results tab.
|
Table L5-1. WSP calibration table for
Manning's n.
|
|
X-sec 60
|
N: 0.030
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N: 0.045
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N:
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N:
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N:
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N:
|
N:
|
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WSL = 92.95
|
92.74
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Xsec 135
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WSL = 92.97
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X-sec 20
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|
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WSL = 93.10
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|
|

Figure L5-1. Water surface profiles resulting
from Manning's n = 0.045.
Increasing the Manning's n from 0.030 to 0.045 raised
the water surface profile at all cross sections. Note that the elevation
for 250 cfs at cross section 60 changed from 92.765 feet to 92.871
feet. Is this close enough? What about the 250 cfs WSL at the other
transects? In this case they are higher than the observed values by
0.081 ft. for transect 135 and 0.066 ft. for transect 201. This would
appear to satisfy the criteria of using a single n value to get the
best fit through the data. However, we have a dilemma. Notice cross
section 60 at 250 cfs. This is the only place where there is a pronounced
rise in observed WSL above the values being predicted by WSP. Also
notice that, at the other calibration flows, the predicted water surface
profile lies above that of the calibration data. Examination of the
cross section shapes, the thalweg profile, or relative transect location
does not reveal a clear reason for the high observed value at cross
section 60. The channel index codes in this study are based on bed
material size. There are a few CI values of 7, but the predominant
value is 6. The predominant value at cross section 0 is also 6. So,
while the bed at cross section 60 may be slightly rougher than at
cross section 0, there is no compelling reason to increase roughness
above that at cross section 0.
In this particular situation, we may suspect an error
in measurement at the high discharge. Following this assumption, we
adjust the n values such that the simulated 250 cfs water surface
profile closely matches the observed values at the upstream two transects.
To accomplish this, reduce the n values in Edit\Cross Sections and
rerun WSP until good agreement is reached. As you make those adjustments,
record n and WSL in Table L5-1. Agreement will occur near n = 0.041
at all cross sections.
With global n = 0.041, the WSL is 0.109 ft. low at
cross section 60, 0.032 ft. high at 135, and 0.005 ft. low at 201.
The 0.109 ft. difference seems large. What kind of error may have
occurred when the measurements were made? One possible scenario is
that the water surface was recorded 0.1 ft. higher than reality. Let
us use that assumption and determine which further local adjustments
to n should be made to reach a WSL of 92.85 ft. instead of 92.95 ft.
Local adjustments to n are best made in pairs stepping
upstream. The Manning's n at the first cross section is changed concurrently
with the value at cross section 60.0 since the predicted water surface
at cross section 60 is dependent on the initial roughness at the down
stream cross section as well as at cross section 60. Changing both
Manning's n values also reduces the chance of obtaining unrealistic
Manning's n values at upstream cross sections during the calibration
process. To reach 92.85, we must raise n at the first two cross sections.
Try a value of 0.042.
Go to \Models\WSL\WSP Options and enter 0.042
for the first two transects. Then set the roughness modifiers to 1.0
for 250 cfs, 1.1 for 139 cfs, and 1.2 for 75.2 cfs, if you have not
already done so, and click Run. Look at the table and longitudinal
plot in ..\Results. Note that while the elevation for 250 cfs
at cross section 60 has now reached 92.848, the elevations upstream
have increased. To get those values back down to within 0.02 ft. of
the observed values will require low n values for cross sections 60
and 135. It is possible to set the n value at cross section 0.0 high
enough that even a low n value at cross section 60 will produce an
elevation of 92.85. However, there is no evidence in this stream that
radical changes in n are justified. Thus, the global value of 0.041
appears to be a reasonable best fit value that causes the simulated
water surface profile at the selected discharge (250 cfs) to "bracket"
the observed values.
Set the n values back to 0.041 for all cross sections and rerun Now
look at the water surface profile (longitudinal) plot. Note that the
observed water surface profiles for the three calibration flows appear
to arch up in the center and become flatter at cross section 201.
This suggests that there is a legitimate increase in roughness between
cross sections 135 and 201. Try modifying the n values for those cross
sections to obtain a better overall fit for the 250 cfs water surface
profile. Be sure to record both the Manning's n values and associated
predictions of the water surface elevations in Table L5-1. An approximate
rule of thumb is that no more than a 5% - 15% change in n values should
occur between transects in an alluvial stream unless there is a topographic
or geologic phenomenon to consider. For example, if large car-sized
boulders densely filled a short section of stream, large changes in
n would be anticipated. That does not appear to be the situation here.
It is important to avoid varying n values merely
for the purpose of obtaining an exact fit of the simulated to observed
water surface profile. When n values vary substantially between transects,
the reliability of extrapolating to higher or lower discharges may
be affected. Generally, n represents the combined roughness of the
bed particle size and bed form (dunes, for example) that resists the
flow of water. Additional losses, such as expansion or contraction
losses, are handled to varying degrees within the WSP model. In some
circumstances, adjustments to n may be used to ensure such losses
are fully represented.
Step 4. Calibration of Roughness Modifiers for
Remaining Calibration Data
Now that Manning's n values have been selected to
approximately reproduce the water surface profile at the high (250
cfs) calibration flow, the next calibration step involves using a
trial-and-error procedure to select RMODs at the remaining calibration
flows which most closely reproduce the longitudinal water surface
profiles at those discharges. Since WSP treats each simulated discharge
independently, calibration of the RMOD for the remaining two calibration
flows can occur at the same time. The RMODs represent constants that
change the magnitude of the Manning's n values at each cross section
while simulating discharges. The RMOD for the calibration flow must
therefore be 1.0 and the RMODs at other flows will be either higher
or lower than 1.0 depending on whether these discharges are higher
or lower than the initial calibration flow. Why?
Recall from Chapter 2 in the manual that roughness
or resistance to flow decreases with increasing discharge. Conversely,
the roughness should increase as flows are reduced. Since the high
calibration flow (i.e., 250 cfs) was used for the initial calibration
of the WSP model, the calibrated Manning's n values alone will be
too low to correctly predict the water surface elevations at the 139
cfs and 75.2 cfs calibration flows. Therefore, the RMODs at these
remaining two calibration flows will need to be greater than 1.0.
Think this through and reread Chapter 3 if it is still unclear why.
This is why we assigned arbitrary RMODs of 1.1 and 1.2 to the 139
cfs and 75.2 cfs discharges earlier.
Select \Models\WSL\WSP Options to display
the RMOD table. Set the RMOD values for 139 cfs and 75.2 cfs to 1.1
and 1.2, respectively if they are not already so set. Then select
..\Results and display the longitudinal plot. Select both Observed
and Simulated water surface elevations and Refresh to
display them. It is convenient to drag the plot to the lower right
of the screen so you can view both the PHABSIM window and plot window
simultaneously. In the plot window, magnify (zoom) the area of water
surface profiles for the calibration discharges. Now click the
Run button to run the models. Click OK when the program
has finished and click the Refresh button in the plot window.
Where do the simulated water surface profiles for 75.2 and 139 cfs
lie in relation to the observed profiles? Are they high or low? Return
to the WSP Options tab.
Figure L5-2 shows the predicted versus observed longitudinal
water surface profiles at the three calibration flows based on our
existing RMODs.
Figure L5-2. Water surface profiles with RMODs
of 1.0, 1.1, and 1.2.
This figure illustrates several key factors in the
calibration of WSP using RMODs. It should be apparent that the predicted
longitudinal profiles for the calibration discharges at 139 cfs and
75.2 cfs 'mimic' the pattern of the water surface profile at the initial
calibration flow of 250 cfs. This should be expected since the only
effect that the roughness modifiers have in the simulation is to change
the magnitude of the Manning's n values and therefore, the relative
differences between the individual cross section Manning's n values
are retained at the other simulated discharges.
In Figure L5-2 (or by viewing \Models\WSL\Results\longitudinal)
you can see that the simulated water surface profiles for 139 and
75.2 cfs are generally lower than the observed profiles for those
discharges. Do not close the graph window, merely click on the PHABSIM
window to move back to it. Remembering that increased roughness will
raise a backwater curve, enter new values for the roughness modifiers
for 139 and 75.2 cfs in the \Models\WSL\WSP Options RMOD table.
Click Run to rerun the models, click OK when the simulation
is done and click the Refresh button to see the results in
the longitudinal profile graph. Continue changing the RMOD values
until you achieve the best overall fit at the discharges of 139 and
75.2 cfs. You may record your iterations of this process in Table
L5-2.
It should also be noted that if either the 75.2 cfs
or 139 cfs flow was selected as the initial calibration discharge,
a close agreement between predicted and observed water surface elevations
at the other flows would be achieved with the right RMOD. This would
be expected given the similarity in the shape of the longitudinal
water surface profiles at both of these discharges. However, neither
of these lower calibration flows would be expected to achieve close
agreement at all cross sections at the high calibration flow given
the difference in the observed longitudinal profile at 250 cfs. This
should reinforce the concept that you should carefully consider which
initial calibration flow to select, or that you should use multiple
calibration flows to see which is best. This determination should
be made in light of both model performance and flow ranges of interest
in the study.
Staying within the 5%-15% guideline described earlier,
try making final small changes to the n values for all cross sections
and to the RMODs to best fit all three water surface profiles
from cross section 0 to cross section 201. Observe the diff
column in the Cal Comparison table and try to find a set of
n values and RMODs that result in not more than a 0.02 ft. difference
at all cross sections and discharges. This final step ensures that
all observed water surface profile data has been used to achieve the
final calibration of WSP over all calibration discharges and over
all cross sections. Table L5-3 gives one possible final calibration
of n values and RMODs. Other combinations of n and RMOD may give a
similar range of WSL calibration errors.
Table L5-2. WSP RMOD calibration table.
Calibration Q = 75.2 X-Sec - 60.0 X-Sec - 135.0 X-Sec 201.0
Target WSL 92.08 92.25 92.36
RMOD: 1.20 92.20 92.23 92.30
RMOD: 1.
RMOD:
RMOD:
RMOD: 1.28
Calibration Q = 139.0 X-Sec - 60.0 X-Sec - 135.0 X-Sec 201.0
Target WSL 92.42 92.59 92.74
RMOD: 1.10 92.51 92.54 92.64
RMOD: 1.
RMOD:
RMOD:
RMOD: 1.22
Table L5-3. A possible WSP calibration.
Cross section n value Discharge RMOD
0.0 0.038 75.2 1.28
60.0 0.038 139 1.23
135.0 0.043 250 1.00
201.0 0.043
Laboratories 3 and 4 demonstrated that neither the
stage-discharge or MANSQ models were able to simulate rational (water
flowing downhill) profiles at the high discharge range. Let us assume
that the current WSP model calibration results are the best that can
be achieved and move to the next step in the calibration process.
Step 5. Estimate the Roughness Modifiers for all
Desired Simulation Discharges
Assuming that our final calibration effort for RMODs
listed in Table L5-2 represents the best compromise in matching the
predicted and observed water surface profiles at the medium and low
calibration discharges, the next step will involve trial-and-error
approximation of a linear log-log relation between n and discharge
or development of a regression between the log10 of the
discharges and log10 of the RMOD values. The resulting
regression equation or approximated relation will then be used to
estimate the roughness modifiers for all remaining discharges to be
simulated in WSP (i.e., 15.0, 30.1, 625.0, and 1250.0). The log regression
is easily accomplished with a spreadsheet program.
Figure L5-3 shows the log-log linear regression results
for the relationship between discharge and roughness modifiers obtained
using a spreadsheet program. The equation is:
|
Log10RMOD = -0.2045*log10Discharge
+ 0.502
|
(5-1)
|
This regression equation was used to generate the
estimated roughness modifiers listed in Table L5-4 for the remaining
simulation flows to be used in the laboratory. Note that the log10
of the discharge must be used in the equation and that the result
is the log10 of the roughness modifier. Therefore, the
correct RMOD estimate is derived by exponentiating the result from
the regression equation as the 'x' in 10x.
Figure L5-3. Log-log plot of RMOD and discharge.
|
Table L5-4. Estimated RMOD values at
simulation discharges.
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|
Simulation discharge
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Estimated RMOD
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15.0
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1.83
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30.1
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1.58
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625.0
|
0.852
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1,250.0
|
0.739
|
Enter these values in the RMOD table in the WSP
Options tab and click the Run button. We now have a water
surface profile for each discharge based on the WSP model. The resulting
profiles can be viewed using ..\Results\longitudinal. If you
have not already done so, include the remaining target discharges
in the simulation by moving to ..\Output Options, placing a
check in all check boxes, and re-running the simulation.
The log-log linear RMOD versus discharge relationship
can be visually approximated by trial-and-error by plotting that relationship
in PHABSIM for Windows. In the WSP Options tab, click the Roughness
Modifier Graph button and the log-log radio button. Prior
to setting RMOD values for the simulation discharges, the graph will
look something like Figure L5-4.
Figure L5-4. Roughness modifier graph.
This plot shows the initial RMODS of 1.0 (log10
of 1 is 0.0) for all simulation discharges and log10 of
1.2, 1.1, and 1.0 for 75.2 cfs, 139 cfs, and 250 cfs respectively.
By displaying this plot and the RMOD table in the ..\WSP Options
tab simultaneously, the user can quickly build a linear RMOD vs.
discharge relationship visually. While not as precise as the regression
approach, this is often an adequate approximation for estimating RMOD
values.
Step 6. Evaluate the Hydraulic Simulations
In order to check the effectiveness of the hydraulic
simulations, we examine the longitudinal profile and calibration error
of the water surface elevations for all our simulated data. In particular,
the performance of WSP at the high-simulated discharges is of interest,
since neither STGQ nor MANSQ were able to produce rational results
above our high calibration flow of 250 cfs.
Zoom in on the water surface profiles for 625 cfs
and 1250 cfs in ..\Results\Longitudinal. Compared to the STGQ
and MANSQ results these profiles show water running downhill at the
high discharges. The WSP model produces rational results for the high-simulated
flows. This would suggest that the WSP model could be used for simulations
above the highest calibration flow (i.e., above 250 cfs).
Now zoom in on the water surface profiles for 15 cfs and 30 cfs. Do
these results also look rational? It does appear that a weak pool
is produced by backwater from cross sections 0.0 and 60. Neither of
those sections shows clear evidence of being a strong control. More
likely, control is the result of the overall resistance of the channel
between those two sections. This condition is often referred to as
channel control and helps explain the observed and simulated water
surface profiles seen here.
You may compare the water surface profiles developed
using WSP and STGQ by starting another copy of PHABSIM and loading
the lab03 SAMPLE data set. Longitudinal plots for both data sets can
be displayed on the screen at once by sizing windows appropriately.
Do not try to load two copies of the same project.
Based on these results, the WSP simulated water surface
elevations will be used for the subsequent steps in the laboratory
exercises.
A final note: We ignored the water surface elevation
at cross section 60 for 250 cfs and assumed it was a measurement error.
What if it was not a measurement error? What would need to be done
differently in this WSP calibration to achieve the "best"
simulation? Specifically, could we stay within the 5%-15% change in
'n' guideline? Could the maximum water surface simulation error be
held to + 0.02 ft.? How would the RMODs change?
To explore these questions you can make a copy of
the project at the present stage using \File\Save As and re-calibrate
assuming that the cross section 60 value is correct.
Laboratory 6. Velocity Modeling - VELSIM
Objectives
The objectives of this laboratory are to explore
various methods for velocity modeling within PHABSIM using the VELSIM
program and to introduce the basic techniques for evaluation of the
effectiveness of velocity simulations.
Programs Used: VELSIM, WSP
Data Files Used: Lab6.phb
Introduction
In this laboratory, different empirical approaches
to simulating velocities are examined. Recall from Chapter 2 of the
manual, that VELSIM can use specific velocity calibration sets for
specific ranges of discharges, and a conveyance area-based velocity
distribution can be developed when no calibration velocities are available.
The 'best' approach can only be determined by evaluating a combination
of available data, model performance, and objectives of the particular
study.
This laboratory explores several different velocity
set combinations and simulation control options within VELSIM to help
the user understand the effects and consequences of selecting a particular
velocity calibration data set and modeling option(s) within VELSIM.
The laboratory is also intended to demonstrate the implications of
selecting a particular water surface elevation model and subsequent
effects during the simulation of velocities in VELSIM. The overall
objective of velocity calibration and simulation is to pick the best
combination of calibration velocity(s) and simulation options to represent
the velocity profiles at each cross section over the range of simulated
flows. The steps in this lab provide a good sequence for velocity
simulation.
Step 1. Evaluate Observed Velocity Profiles
Prior to beginning the modeling efforts, examine
the observed velocity profiles at each cross section for all three
calibration flows provided in Figures L6-1 through L6-4. The velocity
profiles between different cross section geometries are highly variable
as would be expected. Also note, however, that the velocity patterns
at specific cross sections are 'generally' similar at all three calibration
flows, but differences in the location of high versus low velocities
and changes in the transverse patterns of velocities between the different
calibration flows are also evident.
Figure L6-1. Observed velocity distribution
for cross section 0.0.
Figure L6-2. Observed velocity distribution
for cross section 60.0.
Figure L6-3. Observed velocity distribution
for cross section 135.0.
Figure L6-4. Observed velocity distribution
for cross section 201.0.
Step 2. Assign Velocity Calibration Sets for
Simulation of Velocities
Go to \Models\Velocity Simulation\Velocity Calibration
Set Assignments and assign velocity sets as shown in Table L6-1.
|
Table L6-1. Initial velocity set assignments.
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Transect
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Discharges
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15
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30
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75.2
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139
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250
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625
|
1,250
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0
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1
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1
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1
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1
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1
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1
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1
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60
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1
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1
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1
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1
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1
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1
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1
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135
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1
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1
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1
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1
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1
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1
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1
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201
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1
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1
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1
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1
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1
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1
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1
|
Assigning velocity set 1 to all cross sections and
discharges tells the program to use the low calibration discharge
velocity distribution as the template for simulating discharges across
the entire flow range of the study. Later we will reset some or all
of these values and compare the different velocity simulation results
to obtain a final set of assigned calibration sets to use for each
transect and discharge combination in this table.
We can now simulate velocities for all discharges
at all cross sections using the low flow calibration set as the velocity
distribution template. Remember that water surface elevations (WSLs)
were previously established using the WSP program.
Step 3. Velocity Simulations Based on Different
Velocity Calibration Data Sets
Begin by simulating velocities using the low discharge
calibration set as the velocity distribution template. To do this,
click the Run button. When the VELSIM program has completed
its execution. A small message box will announce velocity simulation
is finished. Click OK.
Now click the Results tab and the Cross
section button at its bottom to display cross sectional plots.
Click on 75.2 in the discharges table to display results for 75.2
cfs for cross section 0. Click the check boxes such that a check shows
in all four boxes for Observed WSL, Simulated WSL, Observed Velocities,
and Simulated Velocities. Now click the Refresh
button. The graph should look like Figure L6-10. To view it better,
use the Windows maximize button in the upper right corner of the graph
window. You can now visually compare the observed and simulated velocities
at a discharge of 75.2 cfs for cross section 0 based on using the
75.2 cfs calibration set as the velocity distribution template. Click
on cross section 60 in the box at the top left of the window and then
the Refresh button. The graph changes to display the WSL and
velocity data and simulation results for cross section 60 at 75.2
cfs. In the classroom situation, it would take too long for each student
to make printed copies of all of the plots of observed and to simulate
velocities based on different templates, so the results of using calibration
set 1, calibration set 2, and calibration set 3 for all cross sections
at all discharges are given in Figures L6-10 through L6-45 at the
end of this laboratory.
A cursory examination of these figures shows that
the best fit occurs when the simulated discharge is equal to the calibration
set discharge. So it seems reasonable to use Cal Set 1 for discharges
less than or equal to 75.2 cfs, Cal Set 2 for 139 cfs, and Cal Set
3 for discharges greater than or equal to 250 cfs. Try assigning calibration
sets in that order and run the model again. Figures L6-5 to L6-8 contain
the VAF relationships for the four velocity template runs. These results
will be compared in the next section.
Figure L6-5. Velocity adjustment factor for
calibration flow of 75.2 cfs.

Figure L6-6. Velocity adjustment factor for
calibration flow of 139 cfs.
Figure L6-7. Velocity adjustment factor for
calibration flow of 250 cfs.
Figure L6-8. Velocity adjustment factor for
mixed calibration flow sets.
Step 4. Examine the VAF Relationships and Velocity
Profiles
We will first examine the VAF relationships for each
of the four simulations. Remember, velocity predictions at a simulated
discharge are a function of the Manning's n derived from the calibration
velocities at a single calibration flow. Also recall that VELSIM uses
the VAF to maintain mass balance between simulated and computed discharges.
Since roughness decreases with increasing discharge, VAF's below the
calibration flow should generally be less than 1.0 and greater than
1.0 for flows above the velocity calibration flows. The degree to
which the VAF departs from 1.0 at the velocity calibration flow is
a function of the difference between the calculated discharge and
the 'best estimate of the discharge' as well as the difference between
predicted and observed water surface elevations (see Chapter 2 in
the manual).
In Figure L6-5 (where the 75.2 cfs calibration set
was used to simulate all discharges), all the VAF relationships except
at cross section 0 follow the expected pattern. The relationship at
cross section 0 'suggests' that roughness is decreasing with as the
discharge decreases below 139 cfs, which is counter to expected results.
The remaining cross sections appear to behave 'normally'.
The VAF relationships for all four simulations are
shown in Figures L6-5 to L6-8. We can learn several things by comparing
these figures.
First, it should be apparent that the use of a single
velocity calibration set results in VAF relationships, which are more
'typical' of expected results for all but cross section 0. Use of
a mix of all three velocity sets produces an irregularity between
75.2 and 250 cfs for all but cross section 0. Though the VAF traces
appear to have a break in slope at either 75.2 cfs or 139 cfs and
drop to the value at 250 cfs, they do appear to be ascending with
increased discharge within each range of simulation, e.g. 0.0 - 75.2
cfs and above 250 cfs. As only one discharge was simulated using the
139 cfs template, we do not know if this will hold true for the 139
cfs calibration set without running additional discharges. What do
the other VAF plot suggest?
Note the magnitude of the velocity adjustment factors
using the four different approaches. These results show that the choice
of a particular velocity calibration data set can impact both the
magnitude and functional relationship of the VAF's. As might be expected,
since the WSP modeled water surface elevations were used for these
simulations, the VAF relationship for the high flow velocity set is
'best behaved' over all ranges of simulated discharges. The results
at cross section 0 would suggest that either alternative velocity
simulation options in VELSIM should be attempted, that an alternative
water elevation modeling approach may be required, that a combination
of the two may be warranted, or that the channel conditions warrant
further study.
Although an examination of the VAF relationships
helps in the general diagnostics of the velocity simulations, an examination
of the actual predicted velocities for each vertical for all cross
sections at all simulated discharges must be undertaken to critically
evaluate the simulation results. Actual velocity predictions should
receive more emphasis than 'strict' adherence to an expected pattern
of the VAF relationships in evaluation of the effectiveness of the
velocity simulations.
A careful examination of the results shown in Figures
10 - 45 should reveal several key points about this particular data
set and VELSIM velocity simulations in general. First, the predicted
velocities at a given calibration flow using that calibration flow
velocity set do not exactly reproduce the observed velocities. The
velocities measured at each cross section do not necessarily result
in a computed discharge equal to the best estimate of the discharge
or calibration discharge. Thus, the predicted velocities are adjusted
by the computed VAF to maintain mass balance between the simulated
flow and computed flow at the cross section (see Chapter 3 in the
manual).
The second thing to note is that at a given calibration
flow, using that calibration flow velocity set results in some computational
cells at the stream margin that have predicted velocities where none
were observed. This is due to the discrepancy in the observed and
predicted water surface elevations at each cross section and possible
errors in the original data.
It should also be apparent that the velocity pattern
at the calibration flow used in the simulation is 'replicated' at
all simulation flows. This can result in relatively large discrepancies
between observed and simulated velocities when using for example a
low velocity calibration set to simulate high flows or vice versa.
This can often occur when the velocity profiles change dramatically
between discharges due to channel geometry heterogeneity, especially
due to unobserved conditions upstream of the transect.
Collection of a single high flow velocity data set
for use in modeling should be carefully evaluated based on complexity
of the channel geometry at specific cross sections. If significant
changes in velocity profiles are expected over different ranges of
discharge of interest in a study, additional velocity data sets should
be collected.
The results also suggest that simulation of velocities
higher than an observed calibration velocity data set can be problematic
at some cross sections since VELSIM must 'guess' at a Manning's n
value for computational cells where no observed velocities have been
provided at the velocity calibration flow.
The simulation results for cross section 201.0 also
demonstrate the influence of water surface modeling on the predictions
of velocities with VELSIM. Go to Results\Graphs\Longitudinal Profile
and zoom in on the region encompassing the three calibration discharges.
Note that at cross section 201.0 the WSP model is slightly under-predicting
the water surface elevation at the 139.0 cfs and 75.2 cfs calibration
flows. Now view Results\Graphs\Cross Section and select cross
section 201, discharge 75.2 cfs, observed and simulated WSL and velocities.
At 75.2 cfs VELSIM predicts slightly slower water at the cross section
but one cell on the left bank shows a simulated velocity of 0.236
fps where the calibration velocity was 0.0. This provides enough conveyance
to slightly lower the other velocities. At 139 cfs, however, the simulated
velocities are significantly higher than the observed velocities.
The simulated water surface elevation is 0.001 ft higher than the
observed value, not a significant difference. Yet, the velocities
are slightly higher. Why? Noting the calibration data, we find that
the local discharge was 249 cfs, but the best estimate discharge is
250 cfs. Thus, a VAF slightly greater than 1.0 was needed to achieve
mass balance resulting in a very slight increase in velocities in
spite of the slightly higher WSL.
In general, improving the water surface elevation
predictions for any cross section at the calibration flows would bring
the simulated cross sectional areas closer to the observed values.
This would therefore reduce the VAF adjustments and result in a better
match between observed and predicted velocities at the lower calibration
flows. This can be seen the results at the 250 cfs calibration flow
which identically match the calibration velocities over most of the
cross section. Try simulating additional discharges that match the
local discharges measured at cross sections 60 and 135. Do the simulated
velocity results match the observed values better?
The final water surface elevation simulation using
WSP allowed a very large difference (0.137 ft.) between the observed
and predicted water surface elevation at cross section 60 for the
250 cfs discharge. This was based on the assumption that an error
of at least 0.10 ft. had been made in the water surface measurement
at that discharge. In spite of the large difference in water surface
elevation, the simulated velocities are only slightly lower than the
observed velocities. Two cells at the right of the channel, which
have significant simulated velocities when the measured velocities
were zero, explain the lower velocities. The overall close agreement
in simulated and observed velocities further supports the assumption
of a water surface elevation measurement error.
No single velocity calibration set is guaranteed
to work at all ranges of simulated discharges at all cross sections.
The 3-calibration data set approach would appear to represent the
best compromise at all cross sections for all flow ranges. Selection
of an appropriate velocity set(s) should be carefully considered in
light of model performance and study objectives. These results should
reinforce the importance of accurate water surface elevation modeling
prior to undertaking the velocity modeling in VELSIM. A critical examination
of the velocity modeling can also be used to revise water surface
modeling approaches (for example, what to do with cross section 60)
based on the effectiveness of the velocity predictions at specific
ranges of discharge of importance to a particular study.
Step 5. Revise Water Surface Elevations at Discharges
below 250 cfs Based on MANSQ
The water surface elevation modeling conducted in
Laboratories 3, 4, and 5 indicated that either the VELSIM or MANSQ
model matched the observed water surface elevations at the medium
and low calibration flows. In this step of the laboratory, the WSL
data for each cross section will be updated to use the water surface
elevation predictions derived from the MANSQ model for all simulation
flows below 250 cfs. Table L6-2 lists the water surface elevations
for each cross section that will be used for this part of the laboratory.
|
Table L6-2. MANSQ derived water surface
elevations for each cross section.
|
|
Discharge
|
Cross Section
|
|
|
0.0
|
60.0
|
135.0
|
201.0
|
|
15.0
|
91.37
|
91.46
|
91.68
|
91.67
|
|
30.1
|
91.57
|
91.70
|
91.88
|
91.94
|
|
75.2
|
91.90
|
92.08
|
92.25
|
92.36
|
|
139.0
|
92.21
|
92.43
|
92.59
|
92.71
|
Go to \Models\WSL\Method and set the starting
combination for the WSP backwater at cross section 0.0 for discharges
of 75.2 and 139 cfs to WSP-MANSQ and Run the selection.
Now go to \Models\Velocity and click Run
to rerun the velocity simulation using the new elevations derived
from using MANSQ as the starting point in the WSP backwater calculation.
Compare the VAF relationship in Figure L6-9 with Figure L6-8. Updating
the WSLs at the lower discharge ranges (i.e., below 250 cfs) improves
the VAF relationship at cross section 0.0 by reducing the variation
above a VAF value of 1.0 even though it does not result in transforming
the VAF curve into the desired shape.
Figure L6-9. Velocity adjustment factors using
MANSQ for low flow starting WSLs.
Based on these simulation results, the user would
likely conclude that if only one calibration set is to be used, the
high velocity calibration data set could be used for all ranges of
simulated discharges. Alternatively, the user could also use each
velocity calibration data set over a specific range of simulated discharges
such as the high velocity calibration set for all flows greater than
250 cfs and for flows down to a discharge of 139 cfs. The 139 cfs
velocity calibration data set could then be used to model flow down
to 75.2 cfs and then use the 75.2 cfs velocity calibration data set
for all lower simulated discharges. The choice of modeling strategy
is a matter of professional judgment based on the quality of the available
data. The goal is to produce a simulated velocity distribution that
is as near as possible to that which occurs in the stream. A carefully
kept set of analysis notes explaining why a particular strategy was
selected is strongly advised. PHABSIM for Windows maintains a
History.project name text file that records the order of model
runs. This file can be periodically copied to another file and annotated
as a means of tracking the analysis.
Step 6. Use of the NMAX Option in VELSIM to Control
Velocity Simulations
One of the ways to control velocity simulations in
VELSIM is to restrict the magnitudes of the estimated Manning's n
values. This can be accomplished by using the NMAX or NMIN options.
Restriction of Manning's n values can often improve velocity simulations
in computational cells at the margin of the stream where velocity
calibration data does not exist (i.e., verticals in the channel above
the highest velocity calibration data set). Since velocity simulations
at the stream margins can be controlled, the velocity predictions
at all other verticals are also affected due to the interaction of
conveyance and the VAF's.
Selection of a limit on Manning's n, whether a maximum
or minimum, is a matter of professional judgment. One rational approach
is to examine the calculated Manning's n values at computational cells
along the margins of each cross section for each calibration flow
and select a Manning's n which is an 'average' of these values. Alternative
approaches include the estimation of a Manning's n value using handbook
values (see Chapter 3 in the manual) based on substrate characteristics.
It should be noted that use of an NMAX and/or an NMIN applies to all
computational cells at all cross sections at all flows when running
VELSIM. Therefore, in those instances where substrate characteristics
vary dramatically between cross sections, separate VELSIM data files
containing only selected cross sections may be necessary. In this
laboratory, the NMAX constraint will be applied to the entire data
set over all ranges of simulated discharges.
Go to \Models\Velocity\Options and check the
box labeled Limit Manning's n. Enter an NMAX value of 0.035
and click the Run button. Then view the VAF relation by clicking
the ZVAFF tab and its Graph button.
It is apparent the constraint of Manning's n values
to a maximum of 0.035 has resulted in a reduction in the magnitudes
of the VAF's at all cross sections. This would be expected since lowering
the upper limit on estimated Manning's n should result in higher velocity
predictions. This in turn should decrease the VAF that is derived
from the ratio of simulated discharge over computed discharge. A comparison
of predicted Manning's n and velocities at the first 25 computational
cells at cross section 135 at 15 cfs clearly illustrates the effect
of NMAX on velocity modeling (Table L6-3).
Table L6-3. Comparison of Manning's n and velocity predictions at cross section 135.0 at 15.0 cfs.
NMAX = 0.035 No NAMX
Cell Manning's n Velocity Manning's n Velocity
8 0.035 0.09 0.052 0.07
9 0.035 0.19 0.071 0.11
10 0.035 0.19 0.054 0.14
11 0.035 0.44 0.042 0.43
12 0.035 0.49 0.063 0.32
13 0.035 0.44 0.04 0.45
14 0.035 0.59 0.046 0.52
15 0.035 0.44 0.037 0.48
16 0.035 0.59 0.038 0.64
17 0.035 0.68 0.039 0.72
18 0.035 0.72 0.044 0.68
19 0.035 0.64 0.036 0.71
20 0.035 0.64 0.038 0.69
21 0.035 0.59 0.043 0.56
22 0.035 0.64 0.041 0.63
23 0.035 0.54 0.040 0.55
24 0.035 0.49 0.036 0.56
25 0.035 0.54 0.047 0.48
The overall pattern of velocities generated by limiting
Manning's n needs to be considered before accepting the improved VAF
relation as the best velocity simulation outcome that can be obtained
for velocity simulation. Using \Models\Velocity\Results\Cross Section,
look at the velocity patterns obtained for each cross section at the
three calibration discharges. How well do they match? Do you think
that limiting Manning's n has improved the overall velocity simulation
across all transects over the full range of discharges?
At this point in the analysis, users would need to
determine from the context of their particular application which set
of velocity simulation options and results is best over what target
flow ranges in choosing the appropriate velocity modeling approach.
In some applications it may be desirable to use simulation results
that minimize the error between measured and observed velocities over
the full range of simulations. In other situations, the investigator
may choose to use each single velocity calibration set only over a
specific range of discharges. This is often the case where velocity
patterns vary dramatically across cross section geometries as discussed
in Chapter 2 of the manual.
Step 7. Specifying n values for Problem Areas
Look through Figures L6-10 to L6-45 for those cases
where simulated discharge is equal to the calibration discharge. Note
that some edge conditions are not well simulated due to being dry
at the observed discharge. Table L6-4 contains a summary of the diagnostic
conditions revealed by those figures. Some data errors can be seen
and some velocity simulation problems stand out.
Table L6-4. Summary of data and simulation diagnostic conditions.
Sim Q X-sec Cal Q Figure
75.2 0 75.2 L6-10 Simulated velocity anomaly between 18 and 30, non-
zero observed velocity in dry area on right bank
75.2 60 75.2 L6-13 Zero observed velocities in deep area near right bank
75.2 135 75.2 L6-16 Zero observed velocity in wet cell near right bank
75.2 201 75.2 L6-19 Zero observed velocity in wet cell near left bank
139 0 139 L6-23 Non-zero observed velocity in dry area on right bank
139 60 139 L6-26 Zero observed velocity in wet cell near both banks
139 135 139 L6-29 Zero observed velocities in wet cells near left bank, n
may be too low near left bank
139 201 139 L6-32 Zero observed velocity in wet cells near both banks,
VAF scaling very clear
250 0 250 L6-36 Observed velocity values reversed at right bank?
250 60 250 L6-39 Zero observed velocities in deep area near right bank
250 135 250 L6-42 n appears low at edge on left bank (sim velocity > obs
velocity), odd velocities at 18 and 20
250 201 250 L6-45 n appears low at edge on both banks (sim velocity > obs
velocity)
In \Edit\Cross Sections\Coordinate Data you
can set Manning's n values for specific cells on each cross section.
After examining how VELSIM handles edges (or other parts of the channel)
automatically, you may wish to enter n values for specific cells and
rerun the velocity simulation. Roughness values set for specific cells
apply at all discharges so you must take care that a good n value
for one condition does not perturb the results for other discharges.
Try setting n values on the left bank of cross section 201 for 250
cfs, rerun the simulation, and see how velocity values are affected
at all flows.
The user is encouraged to try additional velocity
simulation options within VELSIM (e.g., placing specific Manning's
n values at specific verticals or using the NMIN option). Examine
the effects on the velocity simulations in terms of both the VAF relationships
and observed versus predicted velocity distributions at each cross
section. Remember that water surface simulations for each cross section
affect the velocity simulations. In some cases water surface errors
can be the main contributing factors for discrepancies between observed
and predicted velocities.
Figure L6-10. Simulated and observed velocity
profile for 75.2 cfs at Xsec 0, Cal Set 75.2.
Figure L6-11. Simulated and observed velocity
profile for 139 cfs at Xsec 0, Cal Set 75.2.
Figure L6-12. Simulated and observed velocity
profile for 250 cfs at Xsec 0, Cal Set 75.2.
Figure L6-13. Simulated and observed velocity
profile for 75.2 cfs at Xsec 60, Cal Set 75.2.

Figure L6-14. Simulated and observed velocity
profile for 139 cfs at Xsec 60, Cal Set 75.2.
Figure L6-15. Simulated and observed velocity
profile for 250 cfs at Xsec 60, Cal Set 75.2.
Figure L6-16. Simulated and observed velocity
profile for 75.2 cfs at Xsec 135, Cal Set 75.2.
Figure L6-17. Simulated and observed velocity
profile for 139 cfs at Xsec 135, Cal Set 75.2.
Figure L6-18. Simulated and observed velocity
profile for 250 cfs at Xsec 135, Cal Set 75.2.
Figure L6-19. Simulated and observed velocity
profile for 75.2 cfs at Xsec 201, Cal Set 75.2.
Figure L6-20. Simulated and observed velocity
profile for 139 cfs at Xsec 201, Cal Set 75.2.
Figure L6-21. Simulated and observed velocity
profile for 250 cfs at Xsec 201, Cal Set 75.2.
Figure L6-22. Simulated and observed velocity
profile for 75.2 cfs at Xsec 0, Cal Set 139.
Figure L6-23. Simulated and observed velocity
profile for 139 cfs at Xsec 0, Cal Set 139.
Figure L6-24. Simulated and observed velocity
profile for 250 cfs at Xsec 0, Cal Set 139.
Figure L6-25. Simulated and observed velocity
profile for 75.2 cfs at Xsec 60, Cal Set 139.
Figure L6-26. Simulated and observed velocity
profile for 139 cfs at Xsec 60, Cal Set 139.
Figure L6-27. Simulated and observed velocity
profile for 250 cfs at Xsec 60, Cal Set 139.
Figure L6-28. Simulated and observed velocity
profile for 75.2 cfs at Xsec 135, Cal Set 139.
Figure L6-29. Simulated and observed velocity
profile for 139 cfs at Xsec 135, Cal Set 139.
Figure L6-30. Simulated and observed velocity
profile for 250 cfs at Xsec 135, Cal Set 139.
Figure L6-31. Simulated and observed velocity
profile for 75.2 cfs at Xsec 201, Cal Set 139.
Figure L6-32. Simulated and observed velocity
profile for 139 cfs at Xsec 201, Cal Set 139.

Figure L6-33. Simulated and observed velocity
profile for 250 cfs at Xsec 201, Cal Set 139.
Figure L6-34. Simulated and observed velocity
profile for 75.2 cfs at Xsec 0, Cal Set 250.
Figure L6-35. Simulated and observed velocity
profile for 139 cfs at Xsec 0, Cal Set 250.
Figure L6-36. Simulated and observed velocity
profile for 250 cfs at Xsec 0, Cal Set 250.
Figure L6-37. Simulated and observed velocity
profile for 75.2 cfs at Xsec 60, Cal Set 250.
Figure L6-38. Simulated and observed velocity
profile for 139 cfs at Xsec 60, Cal Set 250.
Figure L6-39. Simulated and observed velocity
profile for 250 cfs at Xsec 60, Cal Set 250.
Figure L6-40. Simulated and observed velocity
profile for 75.2 cfs at Xsec 135, Cal Set 250.

Figure L6-41. Simulated and observed velocity
profile for 139 cfs at Xsec 135, Cal Set 250.
Figure L6-42. Simulated and observed velocity
profile for 250 cfs at Xsec 135, Cal Set 250.
Figure L6-43. Simulated and observed velocity
profile for 75.2 cfs at Xsec 201, Cal Set 250.
Figure L6-44. Simulated and observed velocity
profile for 139 cfs at Xsec 201, Cal Set 250.
Figure L6-45. Simulated and observed velocity
profile for 250 cfs at Xsec 201, Cal Set 250.