Experimental results of shock trains in rectangular ducts-Reference-Cited by-同舟云学术

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Experimental results of shock trains in rectangular ducts

Published:1992-08-17 Issue: Volume: Page:
ISSN:
Container-title:AlAA 4th International Aerospace Planes Conference
language:
Short-container-title:

Author:

SULLINS G.¹,MCLAFFERTY G.²

Affiliation:

1. Johns Hopkins Univ., Laurel, MD

2. McLafferty Consulting, Inc., North Palm Beach, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-5103

Reference9 articles.

1. Shock Waves in Cylindrical Ducts," AIAA Journal,Vol. 11,No. 10,p. 1404-1408,October 1973.

2. Fig.5 Machnumberdistributionfor M =2. I 12 92-0838

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