EXPERIMENTAL INVESTIGATIONS OF COMPRESSIBLE TURBULENT BOUNDARY LAYER AT VERY HIGH REYNOLDS NUMBERS

被引：13

作者：

MOORE, DR

HARKNESS, J

机构：

来源：

关键词：

D O I：

10.2514/3.2939

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：631 / &

共 15 条

[1] BRINISH PF, 1957, NACATN3979 EFF BLUNT
[2] CLAUSER FH, 1954, 2 S AER BEH TURB BOU
[3] COLES D, 1953, THESIS CALIFORNIA I
[4] FENTER FW, 1959, REE9R2 REP VOUGHT RE
[5] KORKEGI RH, 1964, 17 GUGG AER LAB CAL
[6] LACY JR, 1958, DRL420 DEF RES LAB
[7] LUTHER M, 1955, 20256 REP JET PROP L
[8] MATTING FW, 1960, NASATRR82 TURB SKIN
[9] SMITH DW, 1959, NASATRR26 SKIN FRICT
[10] SKIN FRICTION EXERTED BY A COMPRESSIBLE FLUID STREAM ON A FLAT PLATE
SPALDING, DB
CHI, SW
[J]. AIAA JOURNAL, 1963, 1 (09) : 2160 - 2161