Art
J-GLOBAL ID：200902015616411437   Reference number：89A0273307

A self-adaptive computational method for transonic turbulent flow past a real projectile.

実際の発射体まわりの遷音速乱流のための自己適合計算法
Author (3)：
HSU C-C

About HSU C-C

(Univ. Florida, FL, USA)

About Univ. Florida, FL, USA

, 
SHIAU N-H

About SHIAU N-H

(Univ. Florida, FL, USA)

About Univ. Florida, FL, USA

, 
CHYU W-J

About CHYU W-J

(NASA Ames Research Center, CA, USA)

About NASA Ames Research Center, CA, USA


Material：
ASME. FED (American Society of Mechanical Engineers. Fluids Engineering Division)  (ASME FED (Am Soc Mech Eng Fluids Eng Div))

About ASME. FED (American Society of Mechanical Engineers. Fluids Engineering Division)


Volume： 66  Page： 33-41  Publication year： 1988 
JST Material Number： H0977A  Document type： Article
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)
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projectile

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

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Terms in the title (5)：
Terms in the title
Keywords automatically extracted from the title.
発射体

About 発射体

, 
まわり

About まわり

, 
乱流

About 乱流

, 
自己

About 自己

, 
計算法

About 計算法


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