Art
J-GLOBAL ID：200902076446856934
Reference number：92A0607261
The effects of nozzle exit geometry on forebody vortex control using blowing.
ノズル出口形状が吹出を使用する前部胴体渦制御に及ぼす影響
Author (2)：
,
Material：
Volume：
10th
Issue：
Pt 1
Page：
41-51
Publication year：
1992
JST Material Number：
W0041A
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.
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Aerodynamics of aircrafts
Terms in the title (3)：
Terms in the title
Keywords automatically extracted from the title.
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