Initial value problem for hypersonic boundary layer flows-Reference-Cited by-同舟云学术

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Initial value problem for hypersonic boundary layer flows

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA Computational Fluid Dynamics Conference
language:
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Author:

Fedorov Alexander¹,Tumin Anatoli²

Affiliation:

1. Moscow Inst. of Physics and Technology, Dolgoprudny, Russia

2. Arizona, Univ., Tucson

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2781

Reference37 articles.

1. Schneider, S. P. "Initial Shakedown of the Purdue Mach-6 Quiet-Flow Ludwieg Tube," AIAA Paper 2000-2592,2000.

2. Mack, L. M. "Boundary-Layer Stability Theory,"JPL Report,No.900-277, 1969.

3. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition

Cited by 2 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. An Evaluation of Shock-Capturing Methods on a Hypersonic Boundary Layer Receptivity Problem;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

2. Receptivity to freestream disturbances of Mach 4.5 flow over a flat plate;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

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