Boundary-layer induced pressures on a flat plate in unsteady hypersonic flight
Author:
Affiliation:
1. Case Western Reserve University, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5623
Reference11 articles.
1. Theory of bending multi-layer sandwich plates.
2. Bending theory for multilayer orthotropic sandwich plates.
3. Zien, T. F. and Reshotko, E. "Boundary Layer Induced Pressures on a Flat Plate in Unsteady Hypersonic Flight," AFOSR Scientific Report 69-1229TR, May 1969, Case Western Reserve Univ.
Cited by 3 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. Time dependent shear stress and temperature distribution over an insulated flat plate moving at hypersonic speed;Applied Scientific Research;1971-12
2. Unsteady Boundary-Layer Induced Pressures at Hypersonic Speed;Physics of Fluids;1971
3. Displacement thickness of an unsteady boundary layer with surface mass transfer;International Journal of Heat and Mass Transfer;1970-08
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