Circulation Redistribution in Leading-Edge Vortices with Spanwise Flow
Author:
Affiliation:
1. Queen’s University, Kingston, Ontario K7L 3N6, Canada
Funder
Natural Sciences and Engineering Research Council of Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057030
Reference24 articles.
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4. PolhamusE. C. “A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on a Leading Edge Suction Analogy,” NASA TN D-3767, 1966.
5. Characteristic length scales for vortex detachment on plunging profiles with varying leading-edge geometry
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