Morphing Trailing Edge - Supercritical Airfoil
Автор: Thanaraj T
Загружено: 2018-11-12
Просмотров: 8014
Описание:
CAD design of a morphing trailing edge.
Design was adapted from paper: "Design Aspects of the Elastic Trailing Edge for an Adaptive Wing" - H. P. Monner, D. Sachau, E. Breitbach
Supercrticial airfoil: SC (2) 0614 used as a base design. Airfoil is intended to morph between SC (2) 0614 and SC (2) 0414.
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