| タイトル | Numerical Simulation of a Spatially Evolving Supersonic Turbulent Boundary Layer |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020080634 |
| 著者（英） | Gatski, T. B.; Erlebacher, G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2002-09-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | L-18225
NAS 1.15:211934
NASA/TM-2002-211934 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/91174 |
