| タイトル | Aeroelastic Tailoring via Tow Steered Composites |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140012777 |
| 著者（英） | Stanford, Bret K.; Jutte, Christine V. |
| 発行日 | 2014-09-01 |
| 言語 | eng |
| 内容記述 | The use of tow steered composites, where fibers follow prescribed curvilinear paths within a laminate, can improve upon existing capabilities related to aeroelastic tailoring of wing structures, though this tailoring method has received relatively little attention in the literature. This paper demonstrates the technique for both a simple cantilevered plate in low-speed flow, as well as the wing box of a full-scale high aspect ratio transport configuration. Static aeroelastic stresses and dynamic flutter boundaries are obtained for both cases. The impact of various tailoring choices upon the aeroelastic performance is quantified: curvilinear fiber steering versus straight fiber steering, certifiable versus noncertifiable stacking sequences, a single uniform laminate per wing skin versus multiple laminates, and identical upper and lower wing skins structures versus individual tailoring. |
| NASA分類 | Aerodynamics |
| レポートNO | NF1676L-19338
L-20443
NASA/TM-2014-218517 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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