Optimization for Load Alleviation of Truss-Braced Wing Aircraft with Variable Camber Continuous Trailing Edge Flap

This paper focuses on load alleviation optimization for a high aspect ratio truss braced wing (TBW) aircraft. The TBW aircraft model is based on the Subsonic Ultra Green Aircraft Research (SUGAR) concept developed by Boeing, with the wing structures of the model modified to include a novel aerodynam...

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Bibliographische Detailangaben

Hauptverfasser:	Lebofsky, Sonia, Ting, Eric, Nguyen, Nhan, Trinh, Khanh
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aircraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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