Initiator detonation diffraction studies in pulse detonation engines-Reference-Cited by-同舟云学术

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Initiator detonation diffraction studies in pulse detonation engines

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Sinibaldi J.¹,Brophy C.¹,Li C.²,Kailasanath K.²

Affiliation:

1. Naval Postgraduate School, Monterey, CA

2. Navy Research Lab., Washington, DC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3466

Reference18 articles.

1. Intermittent Detonation as a Thrust-Producing Mechanism

2. 2Eidelman,S.,and Grossmann,W. "Pulsed Detonation Engine: Experimental andTheoretical Review," AIAA Paper 99-1067,1999.

3. 4Kailasanath, K. "Applications of Detonation to Propulsion:A Review,"AIAA Paper 99-1067,1999.

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1. Numerical Simulation of the Influence of Hydrogen Concentration on Detonation Diffraction Mechanism;Energies;2022-11-20

2. High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations;Journal of Propulsion and Power;2017-01

3. Efforts on High-Frequency Pulse Detonation Engines;Journal of Propulsion and Power;2017-01

4. Validation of the Short Kinetic Mechanism for Jet A-Air Detonations;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

5. Thrust Chamber Dynamics and Propulsive Performance of Single-Tube Pulse Detonation Engines;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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