An Improved Multi-Objective Particle Swarm Optimization Method for Rotor Airfoil Design
Author:
Affiliation:
1. Department of Aeronautics & Astronautics, Fudan University, Shanghai 200433, China
2. Rotor Aerodynamics Key Laboratory, China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract
Funder
Open Project of Rotor Aerodynamics Key Laboratory
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/9/820/pdf
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3. Vozhdajev, E., and Golovkine, V. (September, January 30). Current state-of-the-art of TsAGI studies in the area of helicopter aerodynamics. Proceedings of the 21st European Rotorcraft Forum, Moscow, Russia.
4. Aerodynamic design optimization of helicopter rotor blades including airfoil shape for hover performance;Ngoc;Chin. J. Aeronaut.,2013
5. Tatossian, C., and Nadarajah, S. (2007, January 25–28). Optimum shape design of helicopter rotors in forward flight via control theory. Proceedings of the 18th AIAA Computational Fluid Dynamics Conference, Miami, FL, USA.
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