Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

Author:

Stanford Bret,Ifju Peter,Albertani Roberto,Shyy Wei

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference147 articles.

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2. Torres G, Mueller T. Micro aerial vehicle development: design, components, fabrication, and flight testing. In: AUVSI unmanned systems symposium and exhibition, Orlando, FL, July 11–13, 2000.

3. Grasmeyer J, Keenon M. Development of the black widow micro air vehicle. In: AIAA aerospace sciences meeting and exhibit, Reno, NV, January 8–11, 2001.

4. Ifju P, Jenkins D, Ettinger S, Lian Y, Shyy W, Waszak M. Flexible-wing-based micro air vehicles. In: Confederation of European aerospace societies aerodynamics conference, London, UK, June 10–12, 2003.

5. Shkarayev S, Null W, Wagner M. Development of micro air vehicle technology with in-flight adaptive-wing structure. NASA contractor report, CR-213271, 2004.

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