| タイトル | Development of advanced stability theory suction prediction techniques for laminar flow control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780019125 |
| 著者（英） | Srokowski, A. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-06-01 |
| 言語 | eng |
| 内容記述 | The problem of obtaining accurate estimates of suction requirements on swept laminar flow control wings was discussed. A fast accurate computer code developed to predict suction requirements by integrating disturbance amplification rates was described. Assumptions and approximations used in the present computer code are examined in light of flow conditions on the swept wing which may limit their validity. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78N27068 |
| 権利 | No Copyright |
