THEORY OF LAMINAR VISCOUS-INVISCID INTERACTIONS IN SUPERSONIC FLOW

被引：32
作者：
KLINEBERG, JM
LEES, L
机构：
来源：
AIAA JOURNAL | 1969年 / 7卷 / 12期
关键词：
D O I：
10.2514/3.5518
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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页码：2211 / +
页数：1
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共 25 条
[1]  
COHEN CB, 1956, NACA1293 REP
[2]   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
[3]  
CROCCO L, 1955, JAN P C HIGH SPEED A, P75
[4]  
FALKNER VM, 1930, RM1314 BRIT AIR RES
[5]   UPSTREAM INFLUENCE IN VISCOUS INTERACTION PROBLEMS [J].
GARVINE, RW .
PHYSICS OF FLUIDS, 1968, 11 (07) :1413-&
[6]   LAMINAR BOUNDARY-LAYER SEPARATION AND NEAR-WAKE FLOW FOR A SMOOTH BLUNT BODY AT SUPERSONIC AND HYPERSONIC SPEEDS [J].
GRANGE, JM ;
KLINEBER.JM ;
LEES, L .
AIAA JOURNAL, 1967, 5 (06) :1089-&
[7]  
HOLDEN MS, 1965, AI1972A3 CORN AER LA
[8]  
KLINEBERG JM, 1969, AIAA697 PAP
[9]  
KLINEBERG JM, 1968, THESIS CALIFORNIA I
[10]   SUPERSONIC LAMINAR BOUNDARY LAYER ALONG A 2-DIMENSIONAL ADIABATIC CURVED RAMP [J].
KO, DRS ;
KUBOTA, T .
AIAA JOURNAL, 1969, 7 (02) :298-&
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