Variations of flutter mechanism of a span-morphing wing involving rigid-body motions
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference22 articles.
1. A review of morphing aircraft;Barbarino;J Intel Mat Syst Str,2011
2. Morphing aircraft systems: historical perspectives and future challenges;Weisshaar;J Aircraft,2013
3. Design and testing of a pneumatic telescopic wing for unmanned aerial vehicles;Blondeau;J Aircraft,2007
4. Development and testing of a span-extending morphing wing;Vocke;J Intel Mat Syst Str,2011
5. Theoretical and experimental aeroelastic study for folding wing structures;Tang;J Aircraft,2008
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