THE TURBULENT BOUNDARY LAYER ON CHEMICALLY ACTIVE ABLATING SURFACES

被引:5
作者
DENISON, MR
机构
来源
JOURNAL OF THE AEROSPACE SCIENCES | 1961年 / 28卷 / 06期
关键词
D O I
10.2514/8.9041
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:471 / 479
页数:9
相关论文
共 20 条
[1]  
CHAUVIN LT, 1955, NACA RM L55C29
[2]  
DENISON MR, 1958, U166 AER DOC
[3]  
DENISON MR, 1957, U110 AER DOC
[4]  
DENISON MR, 1959, U702 AER DOC
[5]   THE EFFECT OF MASS TRANSFER ON THE COMPRESSIBLE TURBULENT BOUNDARY-LAYER SKIN FRICTION AND HEAT TRANSFER [J].
DORRANCE, WH ;
DORE, FJ .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (06) :404-410
[6]   THE LAMINAR-TURBULENT TRANSITION IN A BOUNDARY LAYER .1. [J].
EMMONS, HW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (07) :490-498
[7]   EXPERIMENTS ON POROUS-WALL COOLING AND FLOW SEPARATION CONTROL IN A SUPERSONIC NOZZLE [J].
GREEN, L ;
NALL, KL .
JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (11) :689-697
[8]  
Karman T., 1930, NACHRICHTEN GESELLSC, P58
[9]  
LEADON BM, 1956, J AERONAUT SCI, V23, P798
[10]  
LEES L, 1958, 3 COMB PROP AGARD CO, P451