Mixing enhancement due to pressure and density gradients generated by expansion waves in supersonic flows-Reference-Cited by-同舟云学术

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Mixing enhancement due to pressure and density gradients generated by expansion waves in supersonic flows

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

Author:

LI C.¹,KAILASANATH K.¹,BOOK D.¹

Affiliation:

1. U.S. Navy, Naval Research Laboratory, Washington, DC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-374

Reference11 articles.

1. Guirguis, R.H., Grinstein, F.F.,Young, T.R., Oran, E.S., Kailasanath, K., Boris, J.P., Mixing Enhancement in Supersonic Shear Layers, AIAA-87-0369

2. A numerical study of mixing enhancement in supersonic reacting flow fields

3. Guirguis, R.H. Mixing Enhancement in Supersonic Shear Layers: 111.Effect of ConvectiveMach Number, AIAA-88-070 1.

4. Li, C. and Kailasanath, K., A Numerical Study of Transverse Jets into Supersonic Flows and Influence of Pressure Waves, AIAA-90-0733.

5. Flux-corrected transport. I. SHASTA, a fluid transport algorithm that works

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. Parametric correlations for generic scramjet combustor ramp injectors;Advanced Measurement and Ground Testing Conference;1996-06-17

2. Advanced injection and mixing techniques for scramjet combustors;Journal of Propulsion and Power;1994-03

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