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INFLUENCE OF THE LEADING-EDGE SHOCK WAVE ON THE LAMINAR BOUNDARY LAYER AT HYPERSONIC SPEEDS

被引：7
作者：
LEES, L
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1956年 / 23卷 / 06期
关键词：
D O I：
10.2514/8.3614
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：594 / &
相关论文
共 8 条
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[2]  
FERRI A, 1954, J AERONAUT SCI, V21, P130
[3]  
HAMMITT AG, 1954, WADC ARDC TR54257
[4]   ON THE BOUNDARY-LAYER EQUATIONS IN HYPERSONIC FLOW AND THEIR APPROXIMATE SOLUTIONS [J].
LEES, L .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (02) :143-145
[5]   HYPERSONIC VISCOUS FLOW OVER AN INCLINED WEDGE [J].
LEES, L .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (11) :794-796
[6]  
LEES L, 1952, PRINCETON U AERO ENG, V195
[7]   ON THE MOTION OF A FLAT PLATE AT HIGH SPEED IN A VISCOUS COMPRESSIBLE FLUID .2. STEADY MOTION [J].
STEWARTSON, K .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (05) :303-309
[8]  
STEWARTSON K, UNPUB
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