Spure Dike: Difference between revisions
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The computational grid size is 152 x 36 and has a variable grid resolution of 0.01 to 0.05 m (Figure 1). The mesh was refined manually near the structure, near the walls within the recirculation zone behind the structure. A constant flux was specified at the inflow boundary and a zero water level at the outflow boundary. | The computational grid size is 152 x 36 and has a variable grid resolution of 0.01 to 0.05 m (Figure 1). The mesh was refined manually near the structure, near the walls within the recirculation zone behind the structure. A constant flux was specified at the inflow boundary and a zero water level at the outflow boundary. | ||
[[Image:SpureDikeGrid2.png|thumb|none| | [[Image:SpureDikeGrid2.png|thumb|none|800px|Figure 1. Computational grid for experiment A1 of Rajaratnam and Nwachukwu (1983) .]] | ||
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==Results== | ==Results== | ||
Flow velocities were measured down stream of the flow structure along 4 transects in the transverse direction and at two arbitrary levels or heights y/y0=0.03 and y/y0=0.85. The velocities from y/y0=0.85 are compared to the calculated depth-averaged velocities and are shown in Figure 2. | Flow velocities were measured down stream of the flow structure along 4 transects in the transverse direction and at two arbitrary levels or heights y/y0=0.03 and y/y0=0.85. The velocities from y/y0=0.85 are compared to the calculated depth-averaged velocities and are shown in Figure 2. |
Revision as of 21:05, 15 October 2010
Experiment Setup
The laboratory flume experiment of Rajaratnam and Nwachukwu (1983) consists of a rectangular 37 x 0.92 m flume with open-channel flow and a thin plate of length 0.1524 m used to simulate a groin-like structure. Here the numerical model is compared to experiment A1 of Rajaratnam and Nwachukwu (1983). For this case, the flow depth and discharge were 0.189 m and 0.0453 m3/sec, respectively.
Model Setup
The computational grid size is 152 x 36 and has a variable grid resolution of 0.01 to 0.05 m (Figure 1). The mesh was refined manually near the structure, near the walls within the recirculation zone behind the structure. A constant flux was specified at the inflow boundary and a zero water level at the outflow boundary.
Results
Flow velocities were measured down stream of the flow structure along 4 transects in the transverse direction and at two arbitrary levels or heights y/y0=0.03 and y/y0=0.85. The velocities from y/y0=0.85 are compared to the calculated depth-averaged velocities and are shown in Figure 2.
Table 1. Goodness of fit statistics for U-velocity, m/s
Transect 1 | Transect 2 | Transect 3 | Transect 4 | |
RMSE | 0.0504 | 0.0690 | 0.0557 | 0.0627 |
RMAE | 0.0239 | 0.0725 | 0.0884 | 0.1038 |
R2 | 0.978 | 0.951 | 0.975 | 0.993 |
References
- Rajaratnam,N. and Nwachukwu, B.A. (1983). "Flow near groin-like structures." J. Hydraulic Eng., 109(3), 463-480.