Drag of vane-type vortex generators in compressible flow
Author:
Affiliation:
1. The University of Texas at Austin, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.30153
Reference9 articles.
1. Measurements of errors caused by misalignment of floating-element skin-friction balances
2. Hoerner, S. F., Fluid Dynamic Drag, 2nd ed., published by author,Midland Park, N. J., 1965, pp.17-14, 16-11.
Cited by 2 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
1. Effect of Submerged Vortex Generators on Shock-Induced Separation in Supersonic Flow;Journal of Aircraft;2009-05
2. An Experimental Study on the Influence of Vortex Generators on the Shock-Induced Boundary Layer Separation at M=1.4;Journal of Applied Mechanics;2009-04-23
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