Comparison of Space Shuttle Hot Gas Manifold analysis to air flow data-Reference-Cited by-同舟云学术

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Comparison of Space Shuttle Hot Gas Manifold analysis to air flow data

Published:1988-07-11 Issue: Volume: Page:
ISSN:
Container-title:24th Joint Propulsion Conference
language:
Short-container-title:

Author:

MCCONNAUGHEY P.¹

Affiliation:

1. NASA, Marshall Space Flight Center, Huntsville,AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-3007

Reference18 articles.

1. Owens, S. F., Mukerjee, T., Przekwas, A. J., and Singhal, A. K. Analysis of the Phase 3 Design Hot Gas Manifold (HGM) and Turnaround (TAD) Duct Flow Fields, CHAM of North America Technical Report CHAM 405011, Huntsville, AL, December 1984.

2. Wang, T. S. and Dakhoul, Y. SSME HGM Data Reduction for Comparative Study, Continuum Technical Report CI-TR-0095, June

3. I1986.

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. Flow characterization of enabling technologies for advanced propulsion development - CFD and cold flow testing and NASA /Marshall Space Flight Center;31st Joint Propulsion Conference and Exhibit;1995-07-10

2. Management of a CFD organization in support of space hardware development;10th Computational Fluid Dynamics Conference;1991-06-24

3. Two-phase flow in cryogenic rocket engine feed systems;25th Joint Propulsion Conference;1989-07-12

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