Flowfield of a 3-D Swept Shock Boundary Layer Interaction in a Mach 2 Flow-Reference-Cited by-同舟云学术

Flowfield of a 3-D Swept Shock Boundary Layer Interaction in a Mach 2 Flow

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Fluid Dynamics Conference
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Author:

Arora Nishul¹,Ali Mohd Y.¹,Alvi Farrukh S.¹

Affiliation:

1. Florida State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3649

Reference22 articles.

1. Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments

2. 3Settles, G. S. and Dolling, D. S., Tacticle Missile Aerodynamics, Vol.104, chap. Swept Shock/Wave Boundary-Layer Interactions,Progressin Astronautics and Aeronautics, AIAA,New York, 1986, pp.291 - 319.

3. Swept shock/boundary-layer interactions - Tutorial and update

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