Experimental and Numerical Study of Micro-Aerial-Vehicle Propeller Performance in Oblique Flow
Author:
Affiliation:
1. KU Leuven, 3000 Leuven, Belgium
2. University of Liège, 4000 Liège, Belgium
3. Université libre de Bruxelles, 1000 Brussels, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033618
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1. Attitude stabilization of a VTOL quadrotor aircraft
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5. Quadrotor Helicopter Flight Dynamics and Control: Theory and Experiment
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