Vortex breakdown on slender sharp-edged wings
Author:
Affiliation:
1. Wichita State University, Wichita, Kansas
2. University of Kansas, Lawrence, Kansas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44247
Reference14 articles.
1. Polhamus, E. C. "A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on a Leading-Edge Suction Analogy/' TN D-3767, 1966, NASA.
2. Stagnation criterion for vortex flows.
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