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Numerical calculations of shock-wave/boundary-layer flow interactions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Huang, P. G. Liou, W. W. |
| Copyright Year | 1994 |
| Description | The paper presents results of calculations for 2-D supersonic turbulent compression corner flows. The results seem to indicate that the newer, improved kappa-epsilon models offer limited advantages over the standard kappa-epsilon model in predicting the shock-wave/boundary-layer flows in the 2-D compression corner over a wide range of corner angles and flow conditions. |
| File Size | 442082 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950019657 |
| Archival Resource Key | ark:/13960/t3cz84v12 |
| Language | English |
| Publisher Date | 1994-08-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Supersonic Flow Turbulent Flow Computational Fluid Dynamics Interactional Aerodynamics Corner Flow Shock Wave Interaction K-epsilon Turbulence Model Flow Characteristics Two Dimensional Flow Separated Flow Boundary Layers Boundary Layer Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
