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

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

Author(s):: M. Nusca ( Army Research Lab, APG, MD )
Publication title:: AIAA meeting papers on disc
Title of ser.:: AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:: 2007
Pub. Year:: 2007
No.:: 2007-5562
Paper no.:: AIAA Paper 2007-5562
Pub. info.:: Reston, Va.: American Institute of Aeronautics and Astronautics
ISSN:: 10877215
Language:: English
Call no.:: A07400/200718 [CD-ROM 2007 Disc 18]
Type:: Technical Paper

Details

TDL ID:	ZA00049510
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	43rd
Conf. info. (Venue):	Cincinnati, OH
Conf. info. (Date):	2007.07.08-2007.07.11
Note for article:	43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-11, 2007

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