Interactional Effect of Propulsive Propeller Location on Counter-Rotating Coaxial Main Rotor
Author:
Affiliation:
1. Dalian University of Technology, 116024 Dalian, People’s Republic of China
2. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Funder
National Natural Science Foundation of China
The Fundamental Research Funds for the Central Universities of China
Aeronautical Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033316
Reference14 articles.
1. The fundamental configuration and design of the compound helicopter
2. Free-Wake Analysis of Tandem, Tilt-Rotor and Coaxial Rotor Configurations
3. Hover Performance Correlation for Full‐Scale and Model‐Scale Coaxial Rotors
4. Rotor Wake Modeling for Flight Dynamic Simulation of Helicopters
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