MEAN AND FLUCTUATING FLOW MEASUREMENTS IN HYPERSONIC BOUNDARY-LAYER OVER A COOLED WALL

被引：39

作者：

LADERMAN, AJ ^{[1
]}

DEMETRIA.A ^{[1
]}

机构：

[1] PHILCO FORD CORP,NEWPORT BEACH,CA 92600

来源：

关键词：

D O I：

10.1017/S0022112074001042

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：121 / &

共 26 条

[1] VISCOUS INTERACTION EFFECTS ON A STATIC PRESSURE PROBE AT M=6 [J].

BEHRENS, W .

[2] THE LAW OF THE WAKE IN THE TURBULENT BOUNDARY LAYER [J].

COLES, D .

[3]

COLES D, 1969, P AFOSR IFP C COMPUT, V2

[4] TURBULENCE MEASUREMENTS IN AN AXISYMMETRIC COMPRESSIBLE WAKE [J].

DEMETRIA.A .

[5] TURBULENT FRONT STRUCTURE OF AN AXISYMMETRIC COMPRESSIBLE WAKE [J].

DEMETRIADES, A .

DOUGHMAN, EL .

[7]

FELLER WV, 1973, AIAA J, V11, P556, DOI 10.2514/3.6791

HOPKINS, EJ ;

INOUYE, M .

[9]

KANE ED, 1950, NACA2210 TECH NOT

[10]

KEMP JH, 1972, D6965 NASA TECH NOT