Unstable lift on an oscillating blade at near stall conditions
Author:
Affiliation:
1. Royal Inst. of Technology, Stockholm, Sweden
2. Volvo Aero Corp., Trollhattan, Sweden
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3749
Reference18 articles.
1. Discrete Vortex Method for Simulating Unsteady Flow
2. Numerical investigation of dynamic stall of an oscillating wing
3. Experimental and numerical investigations of dynamic stall on a pitching airfoil
4. He, L.:Denton, J.; 1991 "An experiment on Unsteady Flow Over an Oscillating Airfoil" ASME91-GT-181
5. Airfoil dynamic stall at constant pitch rate and high Reynolds number
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