Simulated Flowfields in Near-Ground Operation of Single- and Twin-Rotor Configurations
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 100083 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2609
Reference5 articles.
1. Sun, M. “A Study of Helicopter Rotor Aerodynamics in Ground Effect at Low Speeds,” Ph.D. Dissertation,Dept. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ,Aug. 1983.
2. Technical Note: Prediction of the Flow Field of a Rotor in Ground Effect
3. Laminar Flow Analysis of a Rotor in Hover
4. Three Dimensional Analysis of a Rotor in Forward Flight
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