A THEORY OF SHOCK-WAVE BOUNDARY-LAYER INTERACTION

被引：0
作者：
GOODMAN, TR
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 10期
关键词：
D O I：
暂无
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：715 / 716
页数：2
相关论文
共 8 条
[1]   THE INTERACTION OF SHOCK WAVES WITH BOUNDARY LAYERS ON A FLAT SURFACE [J].
BARRY, FW ;
SHAPIRO, AH ;
NEUMANN, EP .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (04) :229-&
[2]  
HOWARTH L, 1948, P CAMB PHILOS SOC, V44, P380
[3]  
KUO YH, 1953, NACA TN2869
[4]  
LEES L, 1949, 143 PRINC U REP
[5]   REFLECTION AT A LAMINAR BOUNDARY LAYER OF A WEAK STEADY DISTURBANCE TO A SUPERSONIC STREAM, NEGLECTING VISCOSITY AND HEAT CONDUCTION [J].
LIGHTHILL, MJ .
QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1950, 3 (03) :303-325
[6]   ON BOUNDARY LAYERS AND UPSTREAM INFLUENCE .2. SUPERSONIC FLOWS WITHOUT SEPARATION [J].
LIGHTHILL, MJ .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1953, 217 (1131) :478-507
[7]  
RITTER A, 1953, NACA TN2868
[8]   INTERACTION BETWEEN PARALLEL STREAMS OF SUBSONIC AND SUPERSONIC VELOCITIES [J].
TSIEN, HS ;
FINSTON, M .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (09) :515-528
1