Effectiveness of leading-edge vortex flaps on 60 and 75 degree delta wings
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44702
Reference4 articles.
Cited by 27 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
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3. Low-Speed Aerodynamic Characteristics of a Delta Wing with Articulated Wing Tips;AIAA AVIATION 2021 FORUM;2021-07-28
4. Plasma control of vortex flow on a delta wing at high angles of attack;Experiments in Fluids;2013-08
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