Unstart of a Supersonic Model Inlet/Isolator Flow Induced by Mass Injection-Reference-Cited by-同舟云学术

Unstart of a Supersonic Model Inlet/Isolator Flow Induced by Mass Injection

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Do Hyungrok¹,Im Seong-kyun¹,Mungal Mark²,Cappelli Mark¹

Affiliation:

1. Stanford University

2. Santa Clara University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-68

Reference26 articles.

1. 1Emami S., Trexler C. A., Auslender A. H., and Weidner J. P. "Experimental investigation of inlet-combustor isolators for a dual-modescramjet at aMach number of4,"NASATechnicalPaper 3502,1995.

2. 2Wieting A. R. "Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine," NASA TN D-8156,1976.

3. Two-dimensional generic inlet unstart detection at Mach 2.5-5.0

4. Unsteady pressure behavior in a ramjet/scramjet inlet

5. Load Oscillations Caused by Unstart of Hypersonic Wind Tunnels and Engines

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