Two-dimensional unsteady leading-edge separation on a pitching airfoil
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08855
2. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12040
Reference50 articles.
1. 'Stepniewski, W., and Keys, C., Rotary-Wing Aerodynamics, Dover, New York, 1984, pp.1-42.
2. Unsteady viscous flow in the vicinity of a stagnation point
3. Boundary-Layer Separation in Unsteady Flow
4. Progress in analysis and prediction of dynamic stall
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