Effect of Unsteady Blade Pitching Motion on Aerodynamic Performance of Microrotorcraft
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, New York 12180-3590
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.6732
Reference17 articles.
1. New Concepts and Perspectives on Micro-Rotorcraft and Small Autonomous Rotary-Wing Vehicles
2. AERODYNAMIC MEASUREMENTS AT LOW REYNOLDS NUMBERS
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