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THEORETICAL MODEL OF NEAR WAKE OF A SLENDER BODY IN SUPERSONIC-FLOW

被引：8
作者：
OHRENBERGER, JT
BAUM, E
机构：
来源：
AIAA JOURNAL | 1972年 / 10卷 / 09期
关键词：
D O I：
10.2514/3.50344
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
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页码：1165 / +
页数：1
相关论文
共 23 条
[1]  
AI DKY, 1967, AIAA6760 PAP
[2]  
BATT RC, 1967, THESIS CALIFORNIA I
[3]   EXPERIMENTAL INVESTIGATION OF LAMINAR NEAR WAKES BEHIND 20 DEGREES WEDGES AT MINFINITY = 6 [J].
BATT, RG ;
KUBOTA, T .
AIAA JOURNAL, 1968, 6 (11) :2077-&
[4]  
BATT RG, 1970, PRIVATE COMMUNICATIO
[5]   INTERACTING SUPERSONIC LAMINAR WAKE CALCULATIONS BY A FINITE DIFFERENCE METHOD [J].
BAUM, E ;
DENISON, MR .
AIAA JOURNAL, 1967, 5 (07) :1224-&
[6]   AN INTERACTION MODEL OF A SUPERSONIC LAMINAR BOUNDARY LAYER ON SHARP AND ROUNDED BACKWARD FACING STEPS [J].
BAUM, E .
AIAA JOURNAL, 1968, 6 (03) :440-&
[7]   RADIAL BASE-PRESSURE GRADIENTS IN LAMINAR FLOW [J].
CASSANTO, JM .
AIAA JOURNAL, 1967, 5 (12) :2278-&
[8]  
CHAPKIS RL, 1967, 19 AGARD C P
[9]  
CHENG SI, 1963, FLOW AROUND ISOLATED
[10]   A MIXING THEORY FOR THE INTERACTION BETWEEN DISSIPATIVE FLOWS AND NEARLY ISENTROPIC STREAMS [J].
CROCCO, L ;
LEES, L .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (10) :649-676
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