Art
J-GLOBAL ID：201602002400925941 Reference number：58A0018320
Transient Temperature and Thermal Stresses in Skin of Hypersonic Vehicle With Variable Boundary Conditions.
超音速航空機表面のいろいろの境界条件における過渡的温度分布と熱応力
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Author (1)：
CHEN S-Y
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Material：
Trans Am Soc Mech Eng (Transactions of the American Society of Mechanical Engineers)
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Volume：
80
Issue：
7
Page：
1389-1394
Publication year：
1958
JST Material Number：
E0270A
Document type：
Article
Country of issue：
United States (USA)
Terms in the title (4)：
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超音速航空機
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,
境界条件
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,
温度分布
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,
熱応力
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