A Parallel Self-Resembled Recursive Method of Simulating Complex Combustion Flow Field in Liquid Rocket Engine Based on Grid Computing

A Parallel Self-Resembled Recursive Method of Simulating Complex Combustion Flow Field in Liquid Rocket Engine Based on Grid Computing

Author(s):

Yang, Q. ( National University of Defence Technology, Changsha, China (prc) )
Zhao, W.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

41st

Pub. Year:

2005

No.:

2005-3737

Paper no.:

AIAA Paper 2005-3737

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200513 [CD-ROM 2005 Disc 13]

Type:

Technical Paper

Details

TDL ID:	ZA00001633
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Tucson, Arizona
Conf. info. (Date):	2005.07.10-2005.07.13

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