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Structural design and verification of an innovative whole adaptive variable camber wing

  • Published:2019-06 Issue: Volume:89 Page:11-18
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Zhao Anmin,Zou Hui,Jin Haichuan,Wen Dongsheng

Funder

Innovation and Entrepreneurship Foundation of the Aviation Innovation Practice Base of Beihang University

Wing Flying Technologies Co., Ltd

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Structural design of an adaptive wing trailing edge for enhanced cruise performance;Pecora,2016

2. Structure design of an innovative adaptive variable camber wing;Zhao;MATEC Web Conf.,2018

3. Overview of the DARPA/AFRL/NASA Smart Wing Phase II program;Kudva;Proc. SPIE,2001

4. Flight test results from a supercritical mission adaptive wing with smooth variable camber;Powers,1992

5. Overview of the DARPA smart wing project;Kudva;J. Intell. Mater. Syst. Struct.,2004
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