AN APPROXIMATE ANALYSIS OF THERMAL CONDUCTION AND RADIATIVE TRANSPORT IN STAGNATION-POINT SHOCK LAYER

被引:5
作者
NEREM, RM
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10.2514/3.3473
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V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:539 / &
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共 8 条
[1]   PRELIMINARY ESTIMATES OF RADIATIVE TRANSFER EFFECTS ON DETACHED SHOCK LAYERS [J].
GOULARD, R .
AIAA JOURNAL, 1964, 2 (03) :494-502
[2]  
HOSHIZAKI H, 1964, P AIAA ENTRY TECHNOL, P65
[3]  
HOWE JT, 1963, TRR159 NASA
[4]   RADIATIVE AND CONVECTIVE HEATING DURING HYPERVELOCITY RE-ENTRY [J].
NEREM, RM ;
STICKFORD, GH .
AIAA JOURNAL, 1964, 2 (06) :1156-1158
[5]  
NEREM RM, 1965, 15 P INT ASTR C, V3, P151
[6]  
OLSTAD WB, 1965, P 1965 HEAT TRANSF F, P138
[7]  
THOMAS PD, 1964, 64434 AIAA PAP
[8]   INVISCID NONADIABATIC FLOW ABOUT BLUNT BODIES [J].
WILSON, KH ;
HOSHIZAK.H .
AIAA JOURNAL, 1965, 3 (01) :67-&