NEWTONIAN FLOW THEORY FOR SLENDER BODIES

被引:43
作者
COLE, JD
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 06期
关键词
D O I
10.2514/8.3875
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:448 / 455
页数:8
相关论文
共 10 条
[1]  
BUSEMANN A, 1933, HDB NATURWISSENSCHAF, P275
[2]  
COURANT, 1946, SUPERSONIC FLOW SHOC
[3]  
EGGERS AJ, 1952, NACA RMA51K27
[4]   LIFT ON INCLINED BODIES OF REVOLUTION IN HYPERSONIC FLOW [J].
GRIMMINGER, G ;
WILLIAMS, EP ;
YOUNG, GBW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (11) :675-690
[5]   ON HYPERSONIC SIMILITUDE [J].
HAYES, WD .
QUARTERLY OF APPLIED MATHEMATICS, 1947, 5 (01) :105-106
[6]  
IVEY HR, 1948, NACA TN1613
[7]   SIMILARITY SOLUTION FOR A SPHERICAL SHOCK WAVE [J].
LATTER, R .
JOURNAL OF APPLIED PHYSICS, 1955, 26 (08) :954-960
[8]  
LEES L, 1955, J AERONAUTICAL SCI
[9]  
Lin S. C., 1954, J APPL PHYS, V25
[10]  
VANDYKE MD, 1954, NACA TN3173