Art

J-GLOBAL ID：200902194088802110   Reference number：96A0646526

Performance Improvement of Impulse Turbine Stage Using F3D Aerodynamic Design.

完全3次元設計による衝動段落の性能向上

Author (4)： TSUTSUMI MASANORI (三菱重工業) ,  MIZUTORI TAKASHI (三菱重工業) ,  TAKENAGA HISAKUNI (三菱重工業) ,  MASUZAWA CHIKAMUNE (三菱重工業)
Material： ターボ機械  (Turbomachinery)
Volume： 24  Issue： 7  Page： 435-440  Publication year： Jul. 1996 
JST Material Number： S0391B  ISSN： 0385-8839  CODEN： TKAICZ  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： turbomachinery ,...
Semi thesaurus term： guide vane

   To see more with JDream III (charged).   {{ this.onShowAbsJLink("http://jdream3.com/lp/jglobal/index.html?docNo=96A0646526&from=J-GLOBAL&jstjournalNo=S0391B") }}

JST classification (1)： Fluid machineries in general  (QD01000G)

Reference (5)：

• DENTON, J. D. An Improved Time Marching Method for Turbomachinery Flow Calculation. 1982, 82-GT-239
• DENTON, J. D. A Method of Calculating Fully Three Dimensional Inviscid Flow Through Any Type of Turbomachine Blade Row. 1983, 1983-06
• NAGAYAMA, T. Turbine Performance Improvement by Full 3-D Design Blades. Mitsubishi Technical Bulletin. 1989, 191, 163
• KOBAYASHI, K. Verification of Flow Pattern for 3D-Designed Blades. 1991, C423/015
• ZWEIFEL, O. The Spacing of Turbomachine Blading Especially with Large Angular Deflection. Brown Boveri Rev. 1945, 32, 12

Terms in the title (4)： 3次元 ,  設計 ,  段落 ,  性能向上