REVERSE TRANSITION AT AN EXPANSION CORNER IN SUPERSONIC-FLOW

被引:40
作者
NARASIMHA, R [1 ]
VISWANATH, PR [1 ]
机构
[1] INDIAN INST SCI,DEPT AERONAUT ENGN,BANGALORE,INDIA
关键词
D O I
10.2514/3.49793
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:693 / 695
页数:3
相关论文
共 15 条
[1]  
ANANDAMURTHY KR, 1958, 434 PRINC U DEP AER
[2]  
BADRINARAYANAN MA, 1969, J FLUID MECH, V35, P225
[3]  
CHAPMAN DR, 1952, NACA1109 REP
[4]  
FULLER L, 1958, ARCRM3064 AER RES CO
[5]  
MORKOVIN MV, 1955, JUN P HEAT TRANSF FL
[6]   RELAMINARIZATION IN HIGHLY ACCELERATED TURBULENT BOUNDARY-LAYERS [J].
NARASIMHA, R ;
SREENIVASAN, KR .
JOURNAL OF FLUID MECHANICS, 1973, 61 (NOV20) :417-447
[7]  
NARASIMHA R, 1974, 74FM10 IND I SCIENC
[8]   APPARENT REVERSE TRANSITION IN AN EXPANSION FAN [J].
PAGE, RH ;
SERNAS, V .
AIAA JOURNAL, 1970, 8 (01) :189-&
[9]   REVERSION OF TURBULENT TO LAMINAR FLOW [J].
PATEL, VC ;
HEAD, MR .
JOURNAL OF FLUID MECHANICS, 1968, 34 :371-&
[10]  
STERNBERG J, 1954, 906 BALL RES LABS RE