Author:
ZENG Lifang,LIU Liu,SHAO Xueming,LI Jun
Subject
Mechanical Engineering,Aerospace Engineering
Reference29 articles.
1. Kress RW. Variable sweep wing design. The evolution of aircraft wing design. Proceedings of the symposium; 1980 Mar 18-19; Dayton, OH, USA. Reston: AIAA; 1980.
2. Aerodynamic research at NACA/NASA Langley related to the use of variable-sweep wings;Spearman,2012
3. Baldelli D, Lee DH, Sanchéz Peña R, et al. Practical modeling, control and simulation of an aeroelastic morphing UAV. 48th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference; 2007 Apr 23-26; Honolulu, Hawaii. Reston: AIAA; 2007.
4. Ivanco T, Scott R, Love M, et al. Validation of the Lockheed Martin morphing concept with wind tunnel testing. 48th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference; 2007 Apr 23-26; Honolulu, Hawaii. Reston: AIAA; 2007.
5. Weisshaar TA. Morphing aircraft technology-new shapes for aircraft design. Meeting proceedings RTO-MP-AVT-141; Neuilly-sur-Seine. France: RTO; 2006. p. 01-1-01-20.
Cited by
6 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献