A NOTE ON THE LAMINAR BOUNDARY LAYER ON A CIRCULAR CYLINDER IN AXIAL INCOMPRESSIBLE FLOW

被引:49
作者
KELLY, HR
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 09期
关键词
D O I
10.2514/8.3151
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:634 / 634
页数:1
相关论文
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[1]   SIMPLIFIED TREATMENT OF THE TURBULENT BOUNDARY LAYER ALONG A CYLINDER IN COMPRESSIBLE FLOW [J].
ECKERT, HU .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (01) :23-&
[2]   SKIN-FRICTION AND HEAT-TRANSFER CHARACTERISTICS OF A LAMINAR BOUNDARY LAYER ON A CYLINDER IN AXIAL INCOMPRESSIBLE FLOW [J].
SEBAN, RA ;
BOND, R .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (10) :671-675