MODEL FOR EDDY CONDUCTIVITY AND TURBULENT PRANDTL NUMBER

被引:58
作者
CEBECI, T [1 ]
机构
[1] DOUGLAS AIRCRAFT CO, AERODYNAM RES GRP, LONG BEACH, CA 90801 USA
来源
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME | 1973年 / 95卷 / 02期
关键词
D O I
10.1115/1.3450031
中图分类号
O414.1 [热力学];
学科分类号
摘要
引用
收藏
页码:227 / 234
页数:8
相关论文
共 25 条
[1]   A FINITE-DIFFERENCE METHOD FOR CALCULATING COMPRESSIBLE LAMINAR AND TURBULENT BOUNDARY LAYERS [J].
CEBECI, T ;
SMITH, AMO .
JOURNAL OF BASIC ENGINEERING, 1970, 92 (03) :523-&
[2]   CALCULATION OF COMPRESSIBLE TURBULENT BOUNDARY LAYERS WITH HEAT AND MASS TRANSFER [J].
CEBECI, T .
AIAA JOURNAL, 1971, 9 (06) :1091-&
[3]   COMPUTATION OF INCOMPRESSIBLE TURBULENT BOUNDARY LAYERS AT LOW REYNOLDS NUMBERS [J].
CEBECI, T ;
MOSINSKIS, GJ .
AIAA JOURNAL, 1971, 9 (08) :1632-+
[4]  
Cebeci T, 1970, AIAA J, V8, P48, DOI [10.2514/3.6079, DOI 10.2514/3.6079]
[5]  
CLAUSER FH, 1956, ADVANCES APPLIED MEC, V4
[6]   EFFECT OF PRANDTL NUMBER ON TEMPERATURE PROFILES FOR HEAT TRANSFER IN TURBULENT PIPE FLOW [J].
GOWEN, RA ;
SMITH, JW .
CHEMICAL ENGINEERING SCIENCE, 1967, 22 (12) :1701-+
[7]  
H. Schlichting, 1968, BOUNDARY LAYER THEOR
[8]  
Hinze J. O., 1959, TURBULENCE
[9]  
JENKINS R, 1951, I HEAT TRANSFER FLUI, P147
[10]  
JOHNSON DS, 1959, T ASME E, V81, P325