A High-Lift Optimization Methodology for the Design of Leading and Trailing Edges on Morphing Wings

Morphing offers an attractive alternative compared to conventional hinged, multi-element high lift devices. In the present work, morphed shapes of a NACA 64A010 airfoil are optimized for maximum lift characteristics. Deformed shapes of the leading and trailing edge are represented through Bezier cur...

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主要な著者:	Charalampos Themistokleous, Nikolaos-Grigorios Markatos, John Prospathopoulos, Vasilis Riziotis, Giorgos Sieros, George Papadakis
フォーマット:	Artigo
言語:	Inglês
出版事項:	MDPI AG 2021-03-01
シリーズ:	Applied Sciences
主題:	high-lift devices morphing design optimization droop nose trailing edge flap
オンライン･アクセス:	https://www.mdpi.com/2076-3417/11/6/2822
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