Strutjet engine performance-Reference-Cited by-同舟云学术

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Strutjet engine performance

Published:1999-08-22 Issue: Volume: Page:
ISSN:
Container-title:9th International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Siebenhaar Adam¹,Campbell Bryan¹,Nguyen Thong¹

Affiliation:

1. Aerojet, Sacramento, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4809

Reference7 articles.

1. Chen,F.F.,Tam,W.F.,Shimp,N.R.,Nonis,R.B."An Innovative Thermal ManagementSystem For a Mach4 to Mach 8 HypersonicScramjetEngine0022, AIAA Paper98-3734,1998.

2. Heiser,W.H.,Pratt,D.T."Isolator-CombustorInteraction in a Dual-Mode Scramjet Engine0022, AMA Paper93-0358,1993.

3. Zucrow,M.J.,Hoffman,J.D.,GasDynamics,Volume 1,JohnWiley andSons,NewYork, 1976.

4. Siebenhaar, A., Bulman, M., Norris, R., and Thompson,M. "Development andTestingof the AerojetStrutjetCombustor0022,AIAA Paper99-4868.

Cited by 1 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. Experimental investigation of combustion mechanisms of kerosene-fueled scramjet engines with double-cavity flameholders;Acta Mechanica Sinica;2011-11-02

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