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The 3-d navier-stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reddy, D. R. |
| Copyright Year | 1991 |
| Description | Three dimensional viscous flow analysis is performed for a configuration where two crossing and glancing shocks interact with a turbulent boundary layer. A time marching 3-D full Navier-Stokes code, called PARC3D, is used to compute the flow field, and the solution is compared to the experimental data obtained at the NASA Lewis Research Center's 1 x 1 ft supersonic wind tunnel facility. The study is carried out as part of the continuing code assessment program in support of the generic hypersonic research at NASA Lewis. Detailed comparisons of static pressure fields and oil flow patterns are made with the corresponding solution on the wall containing the shock/boundary layer interaction in an effort to validate the code for hypersonic inlet applications. |
| File Size | 845456 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910014817 |
| Archival Resource Key | ark:/13960/t4xh4hg7t |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbulent Flow Computational Fluid Dynamics Supersonic Wind Tunnels Pressure Distribution Turbulent Boundary Layer Shock Wave Interaction Hypersonic Inlets Navier-stokes Equation Hypersonics Three Dimensional Flow Flow Distribution Flow Visualization Time Marching Applications Programs Computers Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
