Unsteady Aerodynamic Optimization of Airfoil for Cycloidal Propellers Based on Surrogate Model
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, Shaanxi, People’s Republic of China
2. Shanghai Aircraft Design and Research Institute, 200000 Shanghai, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033649
Reference53 articles.
1. Performance of a Cycloidal Rotor Concept for Micro Air Vehicle Applications
2. Experimental and Numerical Study of Cyclogiro Aerodynamics
3. A Cycloidal Propeller Using Dynamic Lift
4. Development of a Four-Rotor Cyclocopter
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