Performance, Flight Testing of a Shrouded Rotor Micro Air Vehicle in Edgewise Gusts
Author:
Affiliation:
1. University of Maryland, College Park, Maryland, 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031477
Reference29 articles.
1. Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number
2. Ducted propellers—a critical review of the state of the art
3. Aeromechanics and Control of a Shrouded Rotor Micro Air Vehicle in Hover and in Edgewise Flow
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