| タイトル | Prediction of inviscid stagnation pressure losses in supersonic inlet flows |
| 著者（英） | Liu, Ching Shi; Azevedo, David J.; Rae, William J. |
| 著者所属（英） | State Univ. of New York |
| 発行日 | 1990-10-01 |
| 言語 | eng |
| 内容記述 | An effort is made to quantify the stagnation pressure losses associated with shock-wave systems that may be present in such high Mach number flows as those of scramjet hypersonic diffusers. If the shock-related contribution turns out to be much larger than that attributable to viscous effects, a designer could introduce methods for the minimization of the shock system's scale; in particular, the size of the normal shock should be reduced. The angles presently treated may be approached during vehicle maneuvering or other transients. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 91A12903 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/352124 |
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