Asymmetric crossing shock wave-turbulent boundary layer interaction-Reference-Cited by-同舟云学术

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Asymmetric crossing shock wave-turbulent boundary layer interaction

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Knight Doyle,Garrison T,Settles G,Zheltovodov A,Maksimov A,Shevchenko A,Vorontsov S

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-231

Reference50 articles.

1. Casc 2 15' 110 A 97 59 59 0.50 5.29 x 0.51 0.20 0.50 0.77 cast ib 70 110 A in 1 68 49 o.50 734 x 10-5 0.51 0.20 0.48 0.19

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. Experimental investigation of heat transfer characteristic in supersonic flow field on a sharp fin shape;Shock Waves;2009

2. Advances in CFD prediction of shock wave turbulent boundary layer interactions;Progress in Aerospace Sciences;2003-02

3. Two and three-dimensional viscous analyses of high speed inlets and comparison with experimental data;33rd Joint Propulsion Conference and Exhibit;1997-07-06

4. Computation of 3D asymmetric crossing shock wave/turbulent boundary layer interaction using a full Reynolds stress equation turbulence model;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

5. Asymmetric Crossing-Shock-Wave/Turbulent-Boundary-Layer Interaction;AIAA Journal;1995-12

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