Transonic shock - Turbulent boundary layer interaction and incipient separation on curved surfaces
Author:
Affiliation:
1. Massachusetts, University, Amherst, Mass.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1244
Reference35 articles.
1. Iterative solution of transonic flows over airfoils and wings, including flows at mach 1
2. On boundary layers and upstream influence II. Supersonic flows without separation
3. Self-induced separation
Cited by 5 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. Investigation on Transonic Convex-Corner Flows;Journal of Aircraft;2002-11
2. Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments;Sadhana;1988-02
3. Supersonic viscous-inviscid interaction of a swept compression ramp with a turbulent boundary layer;18th Fluid Dynamics and Plasmadynamics and Lasers Conference;1985-07-16
4. Transonic shock interaction with a tangentially injected turbulent boundary layer;Journal of Aircraft;1985-06
5. ANALYTICAL INVESTIGATION OF SWEPT SHOCK-TURBULENT BOUNDARY LAYER INTERACTION I N SUPERSONIC FLOW;17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1984-06-25
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