Art
J-GLOBAL ID：200902052590653200   Reference number：91A0816288

A compressible three-dimensional design method for radial and mixed flow turbomachinery blades.

半径流および混流ターボ機械の羽根の圧縮性3次元設計方法
Author (1)：
ZANGENEH M

About ZANGENEH M

(Univ. Coll. London, London, GBR)

About Univ. Coll. London, London, GBR


Material：
International Journal for Numerical Methods in Fluids  (Int J Numer Methods Fluids)

About International Journal for Numerical Methods in Fluids


Volume： 13  Issue： 5  Page： 599-624  Publication year： Sep. 05, 1991 
JST Material Number： E0241B  ISSN： 0271-2091  CODEN： IJNFDW  Document type： Article
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)
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Keywords indexed to the article.
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subsonic flow

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,...
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JST classification (1)：
JST classification
Category name(code) classified by JST.
High-speed aerodynamics 
(BC03000C)

About High-speed aerodynamics

Terms in the title (6)：
Terms in the title
Keywords automatically extracted from the title.
半径流

About 半径流

, 
ターボ機械

About ターボ機械

, 
羽根

About 羽根

, 
圧縮性

About 圧縮性

, 
3次元

About 3次元

, 
設計方法

About 設計方法


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