Numerical study of shock-wave/boundary layer interactions in premixed hydrogen-air hypersonic flows-Reference-Cited by-同舟云学术

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Numerical study of shock-wave/boundary layer interactions in premixed hydrogen-air hypersonic flows

Published:1991-01-07 Issue: Volume: Page:
ISSN:
Container-title:29th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

YUNGSTER SHAYE¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-413

Reference59 articles.

1. Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary Layers

2. Ferri, A. and Agnone, A.M. "Heat Conduction Controlled Combnstion for Scramjet Applications," AIAA Paper NYU-AA-73-18.

3. Standing oblique detonation wave engine performance

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. Finite element analysis of the Scramaccelerator with hydrogen-oxygen combustion;Journal of Propulsion and Power;1996-03

2. Implicit Navier-Stokes Solver for Three-Dimensional Compressible Flows;AIAA Journal;1992-11

3. Approximate solutions for oblique detonations in the hypersonic limit;AIAA Journal;1992-03

4. Navier-Stokes simulation of the supersonic combustion flowfield in aram accelerator;27th Joint Propulsion Conference;1991-06-24

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