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Numerical simulation of a spatially evolving supersonic turbulent boundary layer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gatski, T. B. Erlebacher, G. |
| Copyright Year | 2002 |
| Description | The results from direct numerical simulations of a spatially evolving, supersonic, flat-plate turbulent boundary-layer flow, with free-stream Mach number of 2.25 are presented. The simulated flow field extends from a transition region, initiated by wall suction and blowing near the inflow boundary, into the fully turbulent regime. Distributions of mean and turbulent flow quantities are obtained and an analysis of these quantities is performed at a downstream station corresponding to Re(sub x)= 5.548 x10(exp 6) based on distance from the leading edge. |
| File Size | 983655 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020080634 |
| Archival Resource Key | ark:/13960/t6xw9cg5f |
| Language | English |
| Publisher Date | 2002-09-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Supersonic Flow Suction Turbulent Flow Direct Numerical Simulation Computational Fluid Dynamics Turbulence Models Flow Distribution Turbulent Boundary Layer Grid Generation Mathematics Supersonic Boundary Layers Leading Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
