Validation of the Short Kinetic Mechanism for Jet A-Air Detonations-Reference-Cited by-同舟云学术

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Validation of the Short Kinetic Mechanism for Jet A-Air Detonations

Published:2007-07-08 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Zaev Ivan,Strelkova Marina,Kirillov Igor,Okun Mikhail,Potapkin Boris,Tangirala Venkat,Dean Anthony,Tentner Adrian

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Pulse detonation propulsion: challenges, current status, and future perspective

2. Direct initiation of detonation with a multi-step reaction scheme

3. 3Brophy, C.M., Sinibaldi, J.O., Netzer, D.W., and Kailasanath, K. "Initiator Diffraction Limits in a Pulse Detonation Engines", Advances in Confined Detonations, edited by G.D. Roy, S.M. Frolov, R.J. Santoro, S.A. Tsyganov,Torus Press, Moscow, Russia, 2002, pp.271-274

Cited by 2 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. From fundamental study to practical application of kerosene in compression ignition engines: An experimental and modeling review;Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering;2019-04-08

2. Determination of Practical Computational Cell Size for Simulation of H2 Air Detonations in Pulse Detonation Engines;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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