| タイトル | Application of stability theory to laminar flow control |
| 著者（英） | Bushnell, D. M.; Hefner, J. N. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1979-07-01 |
| 言語 | eng |
| 内容記述 | The paper summarizes the state-of-the-art for application of stability theory to laminar flow control using suction, wall temperature and/or favorable pressure gradient ('natural laminar flow'). Discussions include current LFC problem areas requiring stability analyses, methods of relating stability theory to transition with results from data and theory comparisons available thus far, and a summary of low disturbance data available for theory calibration on swept wings. Critical issues highlighted are problems peculiar to suction LFC on high performance transonic wings and application of the e-to-the-n-power method to both low and high speed flight data. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79A46691
AIAA PAPER 79-1493 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/425923 |
