A Pulsed Detonation Tube with a Converging-Diverging Nozzle Operating at Different Pressure Ratios-Reference-Cited by-同舟云学术

A Pulsed Detonation Tube with a Converging-Diverging Nozzle Operating at Different Pressure Ratios

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Barbour Ethan¹,Hanson Ronald¹,Morris Chris²,Radulescu Matei³

Affiliation:

1. Stanford University

2. NASA Marshall Space Flight Center

3. Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1307

Reference22 articles.

1. 1Eidelman,S."PulseDetonationEngine-AStatusReviewandTechnologyDevelopmentRoadMap," AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA-97-2740,1997.

2. Eidelman,S.,andYang,X."AnalysisofthePulseDetonationEngineEfficiency,"AIAA/ASME/SAE/ASEEJoint PropulsionConference, AIAA-98-3877,1998.

3. Bratkovich,T.E.,Aarnio,M.J.,Williams,J.T.,andBussing,T.R.A."Anintroductiontopulse detonation rocket engines(PDREs),"AIAA/ASME/SAE/ASEEJointPropulsionConference, AIAA-97-2742,1997.

4. Bussing,T.,andPappas,G."Anintroductiontopulsedetonationengines,"AIAAAerospaceSciencesMeeting,AIAA-94-0263,1994.

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