Pressure induced by weak interaction with unsteady hypersonic boundary layers.-Reference-Cited by-同舟云学术

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Pressure induced by weak interaction with unsteady hypersonic boundary layers.

Published:1969-08 Issue:8 Volume:7 Page:1609-1610
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

RESHOTKO E.¹,RODKIEWICZ C. M.¹

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/10.2514/3.5443

Reference3 articles.

1. Oscillating Airfoils at High Mach Number

2. Rodkiewicz, C. M. and Reshotko, E. "Time-Dependent Hypersonic Viscous Interactions," Scientific Report 67-2451, Case Inst. of Technology FTAS/TR-67-28, Nov. 1967, Air Force Office of Scientific Research.

Cited by 7 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. Hypersonic interactions with surface mass transfer. I - Steady flow over a slender wedge wing;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07

2. Unsteady boundary-layer induced pressures at high Mach numbers;Acta Mechanica;1982-03

3. Unified nonlinear approach to both weak and strong-interaction problems;Acta Mechanica;1975-03

4. Hypersonic Unsteady Compressible Boundary Layer Dependence on Prandtl Number;Physics of Fluids;1972

5. Time dependent shear stress and temperature distribution over an insulated flat plate moving at hypersonic speed;Applied Scientific Research;1971-12

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