Prediction of Hysteresis Associated with the Static Stall of an Airfoil
Author:
Affiliation:
1. Indian Institute of Technology, Kanpur 208 016, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1051
Reference17 articles.
1. Generalized Vortex Lattice Surfaces in Method for Oscillating Lifting Subsonic Flow
2. Generalized Vortex Lattice Method for Planar Supersonic Flow
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