Flowfield Model for a Rectangular Planform Wing beyond Stall
Author:
Affiliation:
1. University of Maryland, College Park, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50846
Reference19 articles.
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5. 5McIntosh, S.C., Jr. "Studies in Unsteady Hypersonic Flow Theory," Ph.D. Dissertation,Stanford Univ., Calif. Aug. 1965.
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