| タイトル | EFFECT OF CONTROL TRAILING-EDGE THICKNESS OR ASPECT RATIO ON THE OSCILLATING HINGE-MOMENT AND FLUTTER CHARACTERISTICS OF A FLAPTYPE CONTROL AT TRANSONIC SPEEDS |
| 本文（外部サイト） | http://hdl.handle.net/2060/19630004006 |
| 著者（英） | Thompson, R. F.; Moseley, W. C., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1958-04-23 |
| 言語 | Other |
| 内容記述 | Control trailing-edge thickness and aspect ratio effect on oscillating hinge-moment and flutter characteristics of flap-type controls |
| NASA分類 | THERMODYNAMICS AND COMBUSTION |
| レポートNO | 63N13882
NACA-RM-L58B25 |
| 権利 | No Copyright |
