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

著者名:
  • Yang, Q. ( National University of Defence Technology, Changsha, China (prc) )
  • Zhao, W.
掲載資料名:
AIAA meeting papers on disc
シリーズ名:
AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
シリーズ巻号:
41st
発行年:
2005
通号:
2005-3737
ペーパー番号:
AIAA Paper 2005-3737
出版情報:
[Reston, Va.]: American Institute of Aeronautics and Astronautics
ISSN:
10877215
言語:
英語
請求記号:
A07400/200513 [CD-ROM 2005 Disc 13]
資料種別:
テクニカルペーパー

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