| タイトル | Evaluation of the Hinge Moment and Normal Force Aerodynamic Loads from a Seamless Adaptive Compliant Trailing Edge Flap in Flight |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160000937 |
| 著者（英） | Lung, Shun-Fat; Ervin, Gregory; Lu, Kerr-Jia; Flick, Pete; Cruz, Josue; Sridhar, Kota; Miller, Eric J. |
| 著者所属（英） | NASA Armstrong Flight Research Center |
| 発行日 | 2016-01-04 |
| 言語 | eng |
| 内容記述 | This presentation describes the interface hinge moments loads collected during the ACTE flights. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AFRC-E-DAA-TN28829 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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