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J-GLOBAL ID：200902062835443113   Reference number：92A0814747

Effect of Streamwise Pressure Gradient on the Supersonic Mixing Layer.

超音速混合層に対する流れ方向圧力勾配の効果
Author (4)：
ABE T

About ABE T

(Inst. Space and Astronautical Science, Kanagawa, JPN)

About Inst. Space and Astronautical Science, Kanagawa, JPN

, 
FUNABIKI K

About FUNABIKI K

(Inst. Space and Astronautical Science, Kanagawa, JPN)

About Inst. Space and Astronautical Science, Kanagawa, JPN

, 
ARIGA H

About ARIGA H

(Musashi Inst. Technology, Tokyo, JPN)

About Musashi Inst. Technology, Tokyo, JPN

, 
HIRAOKA K

About HIRAOKA K

(Tokai Univ., Kanagawa, JPN)

About Tokai Univ., Kanagawa, JPN


Material：
AIAA Journal (American Institute of Aeronautics and Astronautics)  (AIAA J (Am Inst Aeronaut Astronaut))

About AIAA Journal (American Institute of Aeronautics and Astronautics)


Volume： 30  Issue： 10  Page： 2564-2566  Publication year： Oct. 1992 
JST Material Number： C0248C  ISSN： 1533-385X  CODEN： AIAJAH  Document type： Article
Article type： 短報  Country of issue： United States (USA)  Language： ENGLISH (EN)
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scramjet

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,...
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Rocket engines 
(PB02050J)

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Terms in the title (4)：
Terms in the title
Keywords automatically extracted from the title.
超音速

About 超音速

, 
混合層

About 混合層

, 
流れ方向

About 流れ方向

, 
圧力勾配

About 圧力勾配


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