Reacting Flow CFD Model of Throttling in the Army's Impinging Stream Vortex Engine-Reference-Cited by-同舟云学术

Reacting Flow CFD Model of Throttling in the Army's Impinging Stream Vortex Engine

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Nusca Michael,Mathis Nathan,Michaels Scott

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

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2. Thompson, D.M., and Allan, B.D. "Higher Density Impulse for Bipropellant Gel Propulsion Systems Using High DensityFuel and Oxidizer Gels," Proceedings of the 1995 JANNAF Gel Propulsion Technology Symposium, CPIA Pub. 627,Sept.1995,pp.65-74.

3. Chew, W.M., May, D.L., and Thompson, D.M. "Non-Newtonian Rheology of Gelled Propellants," Proceedings ofthe1998JANNAF Propulsion Meeting,CPIA Pub. 675,Vol. 1,July1998,pp.141-149.

4. Thompson, D.M., Wilson, B.F., and Stephenson, W. "Hypergolic Azide Liquid Fuels," Proceedings of the 1999 JANNAF Propellant Development and Characterization Subcommittee Meeting, CPIA Pub.627,Sept. 1999, pp.65-74.

5. Computational Characterization of 2-Azidocycloalkanamines: Notional Variations on the Hypergol 2-Azido-N,N-Dimethylethanamine (DMAZ)

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