| タイトル | Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane: Wind-tunnel investigation of high-angle-of-attack aerodynamic characteristics |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820018341 |
| 著者（英） | Johnson, J. L., Jr.; Newsom, W. A., Jr.; Satran, D. R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-06-01 |
| 言語 | eng |
| 内容記述 | Wing-leading-edge modifications included leading-edge droop and slat configurations having full-span, partial-span, or segmented arrangements. Other devices included wing-chord extensions, fences, and leading-edge stall strips. Good correlation was apparent between the results of wind-tunnel data and the results of flight tests, on the basis of autorotational stability criterion, for a wide range of wing-leading-edge modifications. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 82N26217
NAS 1.60:2011
L-15101
NASA-TP-2011 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/165677 |
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