| タイトル | Optimum full-scale subsonic wind tunnel |
| 著者（英） | Mort, K. W.; Meyn, Larry A.; Soderman, P. T. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1986-03-01 |
| 言語 | eng |
| 内容記述 | The needs and reasons for performing full-scale subsonic research have been studied. Full-scale wind-tunnel requirements are described; recommended size, airspeed, acoustic capabilities, and flow quality are developed; and data-acquisition systems, productivity, automation, and some cost elements are discussed. It is proposed that the optimum full-scale, subsonic wind tunnel be large enough to accommodate aerodynamic and acoustic investigations on most advanced aircraft, which exhibit complex engine/lifting-surface flow-field interactions, including advanced rotorcraft. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 95A60161
AIAA PAPER 86-0732 |
| 権利 | Copyright |
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