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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. date:
2005
Serial:
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

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