Art
J-GLOBAL ID:200902121969352196   Reference number:01A0497668

Effects of Leading Edge Sweep on Unsteady Cavitation in Inducers. 1st Report. Improvements of Cavity Length Due to Forward and Backward Sweep.

インデューサの前縁スウィープが非定常キャビテーションに与える影響 第1報 前進,後退スウィープの効果
Author (5):
Material:
Volume: 67  Issue: 656  Page: 903-910  Publication year: Apr. 25, 2001 
JST Material Number: F0036B  ISSN: 0387-5016  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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Semi thesaurus term:
Thesaurus term/Semi thesaurus term
Keywords indexed to the article.
All keywords is available on JDreamIII(charged).
On J-GLOBAL, this item will be available after more than half a year after the record posted. In addtion, medical articles require to login to MyJ-GLOBAL.

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JST classification (1):
JST classification
Category name(code) classified by JST.
Pumps,various pumping equipment 
Reference (18):
  • NASA Space Vehicle Design Criteria. Liquid Rocket Engine Turbopump Inducers. 1971, SP-8052, 56
  • ACOSTA, A. J. Proc. 2nd Symp. Naval Hydrodyn. 1958, ACR-38, 537-557
  • WRIGHT, M. K. Trans, ASME. 1964, 179-180
  • YOUNG, W. E. Study of Cavitating Inducer Stability. 1972, CD-123939, 58
  • 上條謙二郎. 航空宇宙技術研究所報告. 1973, TR-345
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