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HYPERSONIC VISCOUS FLOW OVER AN INCLINED WEDGE

被引：7
作者：
LEES, L
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1953年 / 20卷 / 11期
关键词：
D O I：
10.2514/8.2850
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：794 / 796
页数：3
相关论文
共 7 条
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LEES, L .
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[2]  
LEES L, 1952, 195 PRINC U AER ENG
[3]   SHOCK-WAVE EFFECTS ON THE LAMINAR SKIN FRICTION OF AN INSULATED FLAT PLATE AT HYPERSONIC SPEEDS [J].
LI, TY ;
NAGAMATSU, HT .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (05) :345-355
[4]  
MASLEN SH, 1952, NACA TN2818
[5]   SURFACE-PRESSURE GRADIENT AND SHOCK-FRONT CURVATURE AT THE EDGE OF A PLANE OGIVE WITH ATTACHED SHOCK FRONT [J].
MUNK, MM ;
PRIM, RC .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (11) :691-695
[6]   A NOTE ON HYPERSONIC VISCOUS FLOW OVER A FLAT PLATE [J].
PAI, SI .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07) :502-504
[7]  
SHEN SF, 1952, J MATH PHYSICS MIT, V3, P192
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