Shock layers and boundary layers in hypersonic flows-Reference-Cited by-同舟云学术

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Shock layers and boundary layers in hypersonic flows

Published:1994-01 Issue:2 Volume:30 Page:95-212
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Cousteix J.,Arnal D.,Aupoix B.,Brazier J.Ph.,Lafon A.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference209 articles.

1. Effect of compressibility on boundary-layer turbulence;Acharya;AIAA J.,1977

2. Higher-order boundary-layer effects on analytic bodies of revolution;Adams,1968

3. Hypersonic and High Temperature Gas Dynamics;Anderson,1989

4. Laminar-turbulent transition problems in supersonic and hypersonic flows;Arnal,1989

5. Prediction based on linear theory;Arnal,1993

Cited by 4 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. Attached High-Speed Viscous Flow;Basics of Aerothermodynamics;2015

2. Numerical simulation of transient hypersonic flow with real gas effects;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

3. Multiquantum Vibrational Deactivation of N2+(v) by Collisions with N2 and O2 at Thermal Energies;The Journal of Physical Chemistry A;1998-07-29

4. Attached High-Speed Viscous Flow;Basics of Aerothermodynamics

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