Subsonic and Transonic Potential Flow over Helicopter Rotor Blades
Author:
Affiliation:
1. U.S. Army Air Mobility Research and Development Laboratory, Ames Directorate, Moffett Field, Calif.
2. New York University, Bronx, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50404
Reference3 articles.
1. Computation of Transonic Flows past Lifting Airfogs and Slender Bodies
2. Transonic Flow about Two-Dimensional Airfoils by Relaxation Procedures
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