Affiliation:
1. University of Florida
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. Wind-Tunnel Testing and Modeling of a Micro Air Vehicle with Flexible Wings
2. Waszak, M.,Jenkins, L., Ifju, P. "Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle," AIAA Paper 2001-4005,2001.
3. Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings
4. Torres, G. E. "Aerodynamics of Low Aspect Ratio Wings at Low Reynolds Numbers with Applications to Micro Air Vehicle Design," Ph.D. Dissertation,Department of Aerospace and Mechanical Engineering, Universityof Notre Dame,South Bend,Indiana,2002.
5. Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings
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8 articles.
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