A UNIFIED ANALYSIS OF SUPERSONIC NONEQUILIBRIUM FLOW OVER A WEDGE .1. VIBRATIONAL NONEQUILIBRIUM

被引:15
作者
LEE, RS
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10.2514/3.2389
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V [航空、航天];
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08 ; 0825 ;
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页码:637 / 646
页数:10
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[1]   ON WEAK INTERACTION OF STRONG SHOCK AND MACH WAVES GENERATED DOWNSTREAM OF THE SHOCK [J].
CHU, BT .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (07) :433-446
[2]  
CLARKE JF, 1960, J FLUID MECH, V5, P577
[3]  
DRESSLER FR, 1961, SHOCK PROFILES HYPER
[4]  
LANDAU L, 1936, Z SOWJETUNION, V10, P34
[5]   PROPAGATION OF WEAK DISTURBANCES IN A GAS SUBJECT TO RELAXATION EFFECTS [J].
MOORE, FK ;
GIBSON, WE .
JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (02) :117-127
[6]  
NAPOLITANO LG, 1960, AEROTECNICA, V40, P151
[7]   SOME ASPECTS OF NONEQUILIBRIUM FLOWS [J].
SEDNEY, R .
JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (03) :189-&
[8]  
SEDNEY R, 1962, AGARD M HIGH TEMPERA
[10]  
VINCENTI WG, 1962, J MECANIQUE, V1, P193