Preliminary modeling of Pulse Detonation Rocket Engines-Reference-Cited by-同舟云学术

Preliminary modeling of Pulse Detonation Rocket Engines

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
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Author:

Cambier J.-L.¹

Affiliation:

1. MSE-TA, Inc., Butte, MT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2659

Reference11 articles.

1. PI"Pulse Detonation TechnologiesAdvance0022, Aviation Week& SpaceTech.,May 4,1998. "Edwards Lab Seeking High-Payoff Technology', Aviation Week and Space Technology,April 5, 1999. S, Tokarcik-Polsky and J.L. Cambier, "Numerical Study of Transient Flow in Shock Tunnels0022, AIAA Journal, vol. 32

2. (1994),971. 141 J.L. Cambier,"Developmentof Numerical

3. Akuowledgments This work was supportedby a contract@AS& 98035) from NASA Mar&all Space Flight Center(MSFC). Thehelp of J. Priceat NASAMSFC, D. Sobel at United Technologies ResearchCenter(UTRC) and T. Kaemming at Boeing Phantom Works (BOPW) is gratefully aknowledged l4L4A99-2659 35"'AL JointPropulsionConference,Los-Angeles,June1999.

4. 4 -15 -10 -5 0

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