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Numerical Simulation of Shock Wave -Turbulent Boundary-Layer Interaction
| Content Provider | Semantic Scholar |
|---|---|
| Author | Shang, J. S. Hankey, W. L. Law, C. Herbert |
| Copyright Year | 1976 |
| Abstract | Numerical solutions of the Navier-Stokes equations are presented for the interactions of a shock wave and a turbulent boundary layer. The turbulent closure is provided by a relaxation eddy viscosity model that approximates the response of turbulence to a severe pressure gradient. The relaxation eddy viscosity model was successfully applied for a series of compression ramp configurations in a previous investigation by the authors. In the present analysis, further verification of the eddy viscosity model is attempted by investigating shock impingement on a turbulent boundary layer. Computations were performed for shock generators varying from 7.93° to 12.17°, at a freestream Mach number of 2.96 and a Reynolds number of 1.2 x 107. Numerical results obtained with MacCormack's scheme were compared with experimental measurements of the surface pressure distribution and the location of the separation and reattachment points. The density distribution throughout the entire interacting flowfield was also compared with experimental results obtained from holographic interferograms. In general, all essential features of the experimental observation were duplicated by the numerical computation. |
| Starting Page | 1451 |
| Ending Page | 1457 |
| Page Count | 7 |
| File Format | PDF HTM / HTML |
| DOI | 10.2514/3.61484 |
| Volume Number | 14 |
| Alternate Webpage(s) | http://ijopaar.com/files/IssueContent/D-A17303-5011.pdf |
| Alternate Webpage(s) | https://doi.org/10.2514/3.61484 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |