Base Flow Phenomena with and without Injection: Experimental Results, Theories, and Bibliography-Reference-Cited by-同舟云学术

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Base Flow Phenomena with and without Injection: Experimental Results, Theories, and Bibliography

Published:1976-01-01 Issue: Volume: Page:7-210
ISSN:
Container-title:Aerodynamics of Base Combustion
language:
Short-container-title:

Author:

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865145.0007.0210

Reference873 articles.

1. Gabeaud (1931, 1949, 1950) obtained a relation between the base pressure and the Mach number of the projectile based upon what he termed "a turbulence theory of residual resistance." The base pressure is given as a function of the freestream velocity by the relation

Cited by 6 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. Detached-Eddy Simulation With Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow;Journal of Fluids Engineering;2002-12-01

2. Study of the intensive combustion in the scramjet engine;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

3. Analysis of Flowfields over Four-Engine DC-X Rockets;Journal of Spacecraft and Rockets;1997-09

4. Analysis of flowfields over four-engine DC-X rockets;32nd Joint Propulsion Conference and Exhibit;1996-07-01

5. Review and development of base pressure and base heating correlations in supersonic flow;Journal of Spacecraft and Rockets;1995-01

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