Affiliation:
1. National Research Council Canada
Publisher
American Institute of Aeronautics and Astronautics
Reference2 articles.
1. An experimental study of dynamic stall on a finite wing
2. Seddon, J. 1960 The flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation. Tech. Rep. 3502. ARC R & M.
Cited by
3 articles.
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