Art
J-GLOBAL ID：200902001972541395   Reference number：85A0124611

A numerical solution for turbulent flow around the leading edge of a film cooled gas turbine blade.

フィルム冷却したガスタービン翼のリーディングエッジ周りの乱流流れの数値解法
Author (3)：
EL-HADIK A A

About EL-HADIK A A

(El-Mansoura Univ., Egypt)

About El-Mansoura Univ., Egypt

, 
AWAD M M

About AWAD M M

(El-Mansoura Univ., Egypt)

About El-Mansoura Univ., Egypt

, 
ARAID F F

About ARAID F F

(El-Mansoura Univ., Egypt)

About El-Mansoura Univ., Egypt


Material：
Proceedings. ASME-JSME Thermal Engineering Joint Conference, 1983, Vol.4  (Proc ASME JSME Therm Eng Jt Conf 1983 Vol 4)

About Proceedings. ASME-JSME Thermal Engineering Joint Conference, 1983, Vol.4


Page： 199-204  Publication year： 1983 
JST Material Number： K19840501  Document type： Proceedings
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)
Thesaurus term：
Thesaurus term/Semi thesaurus term
Keywords indexed to the article.
All keywords is available on JDreamIII(charged).
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gas turbine

About gas turbine

,...
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Gas turbines 
(PB02040Y)

About Gas turbines

Terms in the title (6)：
Terms in the title
Keywords automatically extracted from the title.
フィルム冷却

About フィルム冷却

, 
ガスタービン翼

About ガスタービン翼

, 
リーディングエッジ

About リーディングエッジ

, 
乱流

About 乱流

, 
流れ

About 流れ

, 
数値解法

About 数値解法


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