Unsteady Separation Processes and Leading Edge Vortex Precursors: Pitch Rate and Reynolds Number Influences
Author:
Affiliation:
1. National Wind Technology Center, Golden, Colorado 80401
2. Applied Simulation Technologies, Cape Canaveral, Florida 32920-0883
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3007
Reference27 articles.
1. Progress in analysis and prediction of dynamic stall
2. Unsteady laminar separation: an experimental study
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