3-DIMENSIONAL SUPERSONIC VISCOUS-FLOW OVER A CONE AT INCIDENCE

被引:25
作者
LIN, A
RUBIN, SG
机构
关键词
D O I
10.2514/3.51213
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1500 / 1507
页数:8
相关论文
共 16 条
[1]   NON-NAVIER STOKES VISCOUS-FLOW COMPUTATIONS [J].
DAVIS, RT ;
RUBIN, SG .
COMPUTERS & FLUIDS, 1980, 8 (01) :101-131
[2]  
DAVIS RT, 1976, 1976 P HEAT TRANSF F
[3]  
LIN A, 1981, AFL81957 U CINC DEPT
[4]  
Lin T. C., 1973, Computers & Fluids, V1, P37, DOI 10.1016/0045-7930(73)90025-X
[5]   VISCOUS FLOW OVER A CONE AT MODERATE INCIDENCE .2. SUPERSONIC BOUNDARY-LAYER [J].
LIN, TC ;
RUBIN, SG .
JOURNAL OF FLUID MECHANICS, 1973, 59 (JUL17) :593-620
[6]  
LIN TC, 1981, AIAA810118 PAP
[7]  
LUBARD S, 1975, COMPUTERS FLUIDS, V3, P83
[8]   EXPERIMENTAL AND THEORETICAL STUDY OF SUPERSONIC VISCOUS FLOW OVER A YAWED CIRCULAR CONE [J].
MARCILLAT, J ;
ROUX, B .
AIAA JOURNAL, 1972, 10 (12) :1625-1630
[9]  
MARCILLAT J, 1970, THESIS U PROVINCE MA
[10]  
MCRAE DS, 1976, AIAA7677 PAP