Experimental study of flow field produced when an underexpanded rocket exhausts into cylindrical tube-Reference-Cited by-同舟云学术

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Experimental study of flow field produced when an underexpanded rocket exhausts into cylindrical tube

Published:1973-08-16 Issue: Volume: Page:
ISSN:
Container-title:9th Propulsion Conference
language:
Short-container-title:

Author:

BATSON J.¹,BERTIN J.²

Affiliation:

1. U.S. Army, Missile Command, Huntsville, Ala.

2. Texas, University, Austin, Tex.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1973-1227

Reference6 articles.

1. Ejectors," Advances in Applied Mechanics, Vol.V. Academic Press, Inc.,Ncw York, 1952, pp1-34.

2. Korst,fr. H.,Chow,W. L., and Ztnnwalt,G. W. "Research on Transonic and Supersonic Flow of a Real Fluid at Abrupt Increases in Cross Section", MX Technical Report 392-5,December 1959, University of Illinois.

3. Detailed Analyses for the Base-Pressure Programs (TSABPP-1,2)

Cited by 3 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. The launch-tube flow-field for a vertical launching system;26th Aerospace Sciences Meeting;1988-01-11

2. Onset of massive blow-by - A comparison of cold-gas simulations and flight tests;16th Aerospace Sciences Meeting;1978-01-16

3. The effect of massive blow-by on the initial trajectory of a free-flight rocket;16th Aerospace Sciences Meeting;1978-01-16

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