Small Rotor Design Optimization Using Blade Element Momentum Theory and Hover Tests
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/10.2514/1.45301
Reference26 articles.
1. Development and Testing of the Mentor Flapping-Wing Micro Air Vehicle
2. Design, Analysis and Hover Performance of a Rotary Wing Micro Air Vehicle
3. Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number
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