| タイトル | On the effect of boundary layer growth on the stability of compressible flows |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810024883 |
| 著者（英） | El-Hady, N. M. |
| 著者所属（英） | Old Dominion Univ. |
| 発行日 | 1981-10-01 |
| 言語 | eng |
| 内容記述 | The method of multiple scales is used to describe a formally correct method based on the nonparallel linear stability theory, that examines the two and three dimensional stability of compressible boundary layer flows. The method is applied to the supersonic flat plate layer at Mach number 4.5. The theoretical growth rates are in good agreement with experimental results. The method is also applied to the infinite-span swept wing transonic boundary layer with suction to evaluate the effect of the nonparallel flow on the development of crossflow disturbances. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 81N33426
NASA-CR-3474 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/167919 |
