SARISTU: Adaptive Trailing Edge Device (ATED) design process review
Author:
Funder
European Union
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference73 articles.
1. Morphing Wing Technologies for Large Commercial Aircraft and Helicopter Scenario;Concilio,2017
2. Caselato de Sousa GL, Rocha dos Santos AG, Sanches AC, et al. Airfoil thickness effects on morphing wings. In: AIAA/AHS adaptive structures conference; 2018.
3. Preliminary airfoil design of an innovative adaptive variable camber compliant wing;Li;J Vibroeng,2016
4. Design aspects of the adaptive wing – the elastic trailing edge and the local spoiler bump;Monner;Aeronaut J,2000
5. Development and testing of a span-extending morphing wing;Vocke;J Intell Mater Syst Struct,2011
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