Rocket nozzle lip flow by direct simulation Monte Carlo method
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia
2. NASA Langley Research Center, Hampton, Virginia
3. University of Sydney, Sydney, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25813
Reference5 articles.
Cited by 18 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. Contamination environment resulting from IUS stage II motor post-burn outgassing;SPIE Proceedings;2002-09-06
2. Numerical study of thruster nozzle plume;38th Aerospace Sciences Meeting and Exhibit;2000-01-10
3. Low-density nozzle flow by the direct simulation Monte Carlo and continuum methods;Journal of Propulsion and Power;1995-01
4. Gasdynamic approach to small plumes computation;Journal of Spacecraft and Rockets;1994-07
5. Particle simulations of helium microthruster flows;Journal of Spacecraft and Rockets;1994-03
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