Statistical data
In this section the relevant statistical data for the diffuser computed with Alya is given. The reported data is the one mentioned in Table 2 of the list of desirable quantities (PDF) and also specified here.
The data is available as:
- In CSV (text) format as profiles along characteristic lines of the diffuser
- In CSV (text) format as contours along characteristic planes of the diffuser.
- In HDF5 (binary) format as volumetric data.
Other turbulent statistics
Other relevant statistics from the database are presented in this section. In particular, the turbulent kinetic energy (TKE) and the characteristic length scales (i.e., the Taylor micro-scale and the Kolmogorov length-scale ) are presented in Fig. 17 along some characteristic contours of the diffuser.
Profile data
The profile data is thought to match that of the UFR_4-16_Test_Case and the experimental data. Text files (in CSV format) are provided at the streamwise locations x/h=0, 2, 4, 6, 8, 10, 12, 14, 15.5, 17, 18, 20 and 22 at the following spanwise locations z/B=0.25, 0.5, 0.75 and 0.875. Some of these profiles are also plotted below.
Characteristic Plots of these profiles are:
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Figure 14: Stanford double diffuser, Re=10000. Turbulent kinetic energy (TKE) budget balance obtained with Alya on characteristic lines of the diffuser.
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Contour data
Contour data is also provided to match that of the UFR_4-16_Test_Case and the experimental data. Text files (in CSV format) are provided at the streamwise locations x/h=2, 5, 8 and 15. These contours are also plotted below.
Characteristic plots of these contours are, on positions x/h=2, 5, 8 and 15:
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Figure 15: Stanford double diffuser, Re=10000, validation. Average streamwise velocity contours, Cherry et al. (2008) and Ohlsson et al. (2010) vs data obtained with Alya. The positions of the contour slices are, from top to bottom, x/h=2, 5, 8 and 15.
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Figure 16: Stanford double diffuser, Re=10000, validation. Average streamwise velocity fluctuation contours, Cherry et al. (2008) and Ohlsson et al. (2010) vs data obtained with Alya. The positions of the contour slices are, from top to bottom, x/h=2, 5, 8 and 15.
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Figure 17: Stanford double diffuser, Re=10000. Turbulent kinetic energy (TKE), Taylor microscale and Kolmogorov lengthscale obtained with Alya on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 18: Stanford double diffuser, Re=10000. Reynolds normal stresses (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 19: Stanford double diffuser, Re=10000. Reynolds shear stresses (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Contour plots of the Reynolds stress equations are given on positions x/h=2, 5, 8 and 15 for each of the budget terms and the residuals of the equation:
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Figure 20: Stanford double diffuser, Re=10000. Production term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 21: Stanford double diffuser, Re=10000. Production term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 22: Stanford double diffuser, Re=10000. Convection term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 23: Stanford double diffuser, Re=10000. Convection term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 24: Stanford double diffuser, Re=10000. Turbulent diffusion D1 term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 25: Stanford double diffuser, Re=10000. Turbulent diffusion D1 term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 26: Stanford double diffuser, Re=10000. Turbulent diffusion D2 term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 27: Stanford double diffuser, Re=10000. Turbulent diffusion D2 term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 28: Stanford double diffuser, Re=10000. Turbulent diffusion D3 term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 29: Stanford double diffuser, Re=10000. Turbulent diffusion D3 term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 30: Stanford double diffuser, Re=10000. Pressure strain term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 31: Stanford double diffuser, Re=10000. Pressure strain term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 32: Stanford double diffuser, Re=10000. Dissipation term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 33: Stanford double diffuser, Re=10000. Dissipation term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 34: Stanford double diffuser, Re=10000. Residual term of the Reynolds stress budget (from left to right 11, 22, 33) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Figure 35: Stanford double diffuser, Re=10000. Residual term of the Reynolds stress budget (from left to right 12, 13, 23) on contour slices located, from top to bottom, at x/h=2, 5, 8 and 15.
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Volume data
Volumetric data on the statistics computed for the whole computational domain are provided here. For more information regarding the storage format, please refer to the storage format guidelines.
The available files are:
Additional data
No additional data yet.
Contributed by: Oriol Lehmkuhl, Arnau Miro — Barcelona Supercomputing Center (BSC)
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