Measurement of Thrust and Lift Forces Associated With Drag of Compliant Flapping Wing for Micro Air Vehicles Using a New Test Stand Design
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.1007/s11340-009-9270-5.pdf
Reference17 articles.
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3. Madangopal R, Khan ZA, Agrawal SK (2006) Energetics-based design of small flapping-wing micro air vehicles. IEEE/ASME Transactions on Mechatronics, 11 (4)
4. Galinski C, Zbikowski R (2007) Materials challenges in the design of an insect-like flapping wing mechanism based on a four-bar linkage. Mater Des 28(3):783–796
5. Cox A, Monopoli D, Cveticanin D, Goldfarb M, Garcia E (2002) The development of elastodynamic components for piezoelectrically actuated flapping micro-air vehicles. J Intell Mater Syst Struct 13(9):611–615
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