BOUNDARY-LAYER VELOCITY DISTRIBUTION IN TURBULENT SWIRLING PIPE FLOW

被引：0

|

作者：

BACKSHAL.RG

LANDIS, F

机构：

来源：

MECHANICAL ENGINEERING | 1969年 / 91卷 / 10期

关键词：

D O I：

暂无

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

收藏

页码：72 / &

相关论文

共 50 条

[1] BOUNDARY-LAYER VELOCITY DISTRIBUTION IN TURBULENT SWIRLING PIPE FLOW
BACKSHALL, RG
LANDIS, F
[J]. JOURNAL OF BASIC ENGINEERING, 1969, 91 (04): : 728 - +
[2] VELOCITY DISTRIBUTION IN TURBULENT OSCILLATORY BOUNDARY-LAYER
YOU, ZJ
WILKINSON, DL
NIELSEN, P
[J]. COASTAL ENGINEERING, 1992, 18 (1-2) : 21 - 38
[3] TEMPERATURE DISTRIBUTION IN TURBULENT BOUNDARY-LAYER IN A CIRCULAR PIPE
HISHIDA, M
NAGANO, Y
NAKAMURA, Y
[J]. BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1978, 21 (157): : 1175 - 1184
[4] BOUNDARY-LAYER VELOCITY PROFILES IN A SWIRLING CONVERGENT FLOW FIELD
HOULIHAN, TM
HORNSTRA, DJ
[J]. JOURNAL OF FLUID MECHANICS, 1972, 52 (MAR28) : 357 - &
[5] VELOCITY PROFILE IN BOUNDARY-LAYER OF TURBULENT STRATIFIED FLOW
ANISIMOVA, EP
POBORCHAYA, LV
SPERANSKAYA, AA
[J]. IZVESTIYA AKADEMII NAUK SSSR FIZIKA ATMOSFERY I OKEANA, 1978, 14 (10): : 1110 - 1114
[6] NEAR WALL VELOCITY DISTRIBUTION OF TURBULENT SWIRLING FLOW IN CIRCULAR PIPE
KITO, O
KATO, T
[J]. BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1984, 27 (230): : 1659 - 1666
[7] INVERSE SOLUTION PROCEDURE FOR TURBULENT SWIRLING BOUNDARY-LAYER COMBUSTION FLOW
LILLEY, DG
CHIGIER, NA
[J]. JOURNAL OF COMPUTATIONAL PHYSICS, 1972, 9 (02) : 237 - &
[8] Confined Boundary-Layer Flashback Flame Dynamics in a Turbulent Swirling Flow
Novoselov, Alex G.
Ebi, Dominik
Noiray, Nicolas
[J]. AIAA JOURNAL, 2023, 61 (04) : 1548 - 1554
[9] DIFFUSION OF MACROMOLECULAR SOLUTIONS IN A TURBULENT BOUNDARY-LAYER OF A CYLINDRICAL PIPE .5. VELOCITY PROFILES AND TURBULENT INTENSITIES IN THE BOUNDARY-LAYER
BUES, M
REITZER, H
TEITGEN, R
[J]. RHEOLOGICA ACTA, 1988, 27 (05) : 512 - 517
[10] Similarities and differences of turbulent boundary-layer, pipe and channel flow
Nieuwstadt, FTM
Bradshaw, P
[J]. BOUNDARY-LAYER SEPARATION IN AIRCRAFT AERODYNAMICS: DEDICATED TO PROFESSOR J.L. VAN INGEN, 1997, : 15 - 22

← 1 2 3 4 5 →