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The Scientific World Journal
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2013
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Article
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Tab 1
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Research Article
Investigation of the Effects of Length to Depth Ratio on Open Supersonic Cavities Using CFD and Proper Orthogonal Decomposition
Table 1
Numerical and experimental parameters for the preliminary CFD study.
Total pressure
66.4 kPa
Total temperature
218 K
Mach number
1.5
Reynolds number
Cavity length
0.12065 m
Cavity depth
0.0238 m
Boundary layer thickness
0.0051 m