| タイトル | Real gas effects on the numerical simulation of a hypersonic inlet |
| 著者（英） | Kunik, W. G.; Ng, W.-F.; Benson, T. J. |
| 著者所属（英） | NASA Lewis Research Center|Virginia Polytechnic Inst. and State Univ. |
| 発行日 | 1986-08-01 |
| 言語 | eng |
| 内容記述 | The present use of a parabolized Navier-Stokes solver to accurately simulate the flowfield in a supersonic inlet yields good agreement between numerical analysis and experiment for a Mach 7.4 inlet under cruise conditions, with an internal compression ratio of 8. The significance of real gas effects on the performance calculation of a hypersonic inlet is demonstrated, with small changes in the ratio of specific heats resulting in a substantial change in the calculated pitot pressure ratio. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 86A46324 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/383373 |
