Utility of Computational Modeling for the Study of Combustion Instability in Small MMH-NTO Liquid Rocket Engines-Reference-Cited by-同舟云学术

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Utility of Computational Modeling for the Study of Combustion Instability in Small MMH-NTO Liquid Rocket Engines

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

Nusca Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

1. Michaels, R.S., and Wilson, B.F. "The Low L/D Vortex Engine for Gel Propulsion," Proceedings of the 1995 JANNAFGelPropulsionTechnologySymposium,CPIA Pub.627,Sept.1995,pp.9-16.

Cited by 4 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. Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine;International Journal of Aerospace Engineering;2020-07-04

2. Experimental and quantum mechanics investigations of early reactions of monomethylhydrazine with mixtures of NO2 and N2O4;Combustion and Flame;2013-05

3. Numerical Simulations of Gel Propellant Flow Through Orifices;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

4. Utility of Computational Modeling for the Study of Combustion Instability in Small MMH-NTO Liquid Rocket Engines;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

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