AN APPROXIMATE SOLUTION OF THE DIRECT SUPERSONIC BLUNT-BODY PROBLEM FOR ARBITRARY AXISYMMETRIC SHAPES

被引:21
作者
TRAUGOTT, SC
机构
来源
JOURNAL OF THE AEROSPACE SCIENCES | 1960年 / 27卷 / 05期
关键词
D O I
10.2514/8.8540
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:361 / 370
页数:10
相关论文
共 23 条
[11]   INVISCID HYPERSONIC FLOW OVER BLUNT-NOSED SLENDER BODIES [J].
LEES, L ;
KUBOTA, T .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (03) :195-202
[12]   STAGNATION POINT OF A BLUNT BODY IN HYPERSONIC FLOW [J].
LI, TY ;
GEIGER, RE .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (01) :25-32
[13]  
LOVE ES, 1957, NACA TN4170
[14]   INVISCID HYPERSONIC FLOW PAST BLUNT BODIES [J].
MASLEN, SH ;
MOECKEL, WE .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (09) :683-693
[15]  
MOECKEL WE, 1949, NACA TN1921
[16]  
MOECKEL WE, 1950, NACA RM E50DO5
[17]  
OLIVER RE, 1956, J AERONAUT SCI, V23, P177
[18]  
SEDNEY R, 1957, J AERONAUT SCI, V24, P630
[19]   SUPERSONIC FLOW AROUND BLUNT BODIES [J].
SERBIN, H .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (01) :58-59
[20]  
TRAUGOTT SC, 1958, RR13 MART CO RES REP