Numerical Investigation of unsteady inlet flow fields-Reference-Cited by-同舟云学术

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Numerical Investigation of unsteady inlet flow fields

Published:1984-01-09 Issue: Volume: Page:
ISSN:
Container-title:22nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HSIEH T.¹,WARDLAW, JR. A.¹,COLLINS P.¹,COAKLEY T.²

Affiliation:

1. U.S. Naval Surface Weapons Center, Silver Spring, MD

2. NASA, Ames Research Center,Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-31

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 measurements of the flow in a scramjet inlet at Mach 4;Journal of Propulsion and Power;1990-11

2. Numerical simulation and comparison with experiment for self-excitedoscillations in a diffuser flow;AIAA Journal;1987-07

3. A second order flux split scheme for the unsteady 2-D Euler equations on arbitrary meshes;8th Computational Fluid Dynamics Conference;1987-06-09

4. Downstream boundary effects on the frequency of self-excited oscillations in transonic diffuser flows;25th AIAA Aerospace Sciences Meeting;1987-03-24

5. Concept and technique for probing channel flows with abrupt perturbations;24th Aerospace Sciences Meeting;1986-01-06

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