THE EFFECT OF MASS TRANSFER ON THE COMPRESSIBLE TURBULENT BOUNDARY-LAYER SKIN FRICTION AND HEAT TRANSFER

被引：34

作者：

DORRANCE, WH

DORE, FJ

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 06期

关键词：

D O I：

10.2514/8.3050

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：404 / 410

页数：7

共 10 条

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[4] MICKLEY HS, 1952, HEAT MASS MOMENTUM T
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[7] SCHOENHERR KE, 1932, T SNAME, V40, P279
[8] TURBULENT BOUNDARY LAYER IN COMPRESSIBLE FLUIDS
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[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (03): : 145 - &
[9] HEAT TRANSFER IN LAMINAR COMPRESSIBLE BOUNDARY LAYER ON A POROUS FLAT PLATE WITH FLUID INJECTION
YUAN, SW
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (12): : 741 - 748
[10] 1951, PROJECT SQUID SEMIAN, P47