| タイトル | Survey of needs and capabilities for wind tunnel testing of dynamic stability of aircraft at high angles of attack |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730013474 |
| 著者（英） | Orlik-Ruckemann, K. J. |
| 著者所属（英） | National Aeronautical Establishment |
| 発行日 | 1973-01-01 |
| 言語 | eng |
| 内容記述 | A survey was conducted relative to future requirements for dynamic stability information for such aerospace vehicles as the space shuttle and advanced high performance military aircraft. High-angle-of-attack and high-Reynolds number conditions were emphasized. A review was made of the wind-tunnel capabilities in North America for measuring dynamic stability derivatives, revealing an almost total lack of capabilities that could satisfy these requirements. Recommendations are made regarding equipment that should be constructed to remedy this situation. A description is given of some of the more advanced existing capabilities, which can be used to at least partly satisfy immediate demands. |
| NASA分類 | FACILITIES, RESEARCH, AND SUPPORT |
| レポートNO | 73N22201
NASA-CR-114583 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199506 |
