CALCULATION OF COMPRESSIBLE TURBULENT BOUNDARY LAYERS WITH HEAT AND MASS TRANSFER

被引：42

作者：

CEBECI, T

机构：

来源：

关键词：

D O I：

10.2514/3.49920

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1091 / &

共 25 条

[1] BARTLE ER, 1962, 1962 P HEAT TRANSF F
[2] SOLUTION OF INCOMPRESSIBLE TURBULENT BOUNDARY-LAYER EQUATIONS WITH HEAT TRANSFER
CEBECI, T
SMITH, AMO
MOSINSKI.G
[J]. JOURNAL OF HEAT TRANSFER, 1970, 92 (01): : 133 - &
[3] A FINITE-DIFFERENCE METHOD FOR CALCULATING COMPRESSIBLE LAMINAR AND TURBULENT BOUNDARY LAYERS
CEBECI, T
SMITH, AMO
[J]. JOURNAL OF BASIC ENGINEERING, 1970, 92 (03): : 523 - &
[4] LAMINAR AND TURBULENT INCOMPRESSIBLE BOUNDARY LAYERS ON SLENDER BODIES OF REVOLUTION IN AXIAL FLOW
CEBECI, T
[J]. JOURNAL OF BASIC ENGINEERING, 1970, 92 (03): : 545 - &
[5] CEBECI T, 1970, AIAA J, V8, P1973
[6] CEBECI T, 1968 P AFOSRIFP STAN, V1, P346
[7] CEBECI T, 1970, MDCJ097301 REP
[8] Cebeci T, 1970, AIAA J, V8, P48, DOI [10.2514/3.6079, DOI 10.2514/3.6079]
[9] CEBECI T, TO BE PUBLISHED
[10] CEBECI T, 1970, 1970 ASME SPAC TECHN