Cross Flows in Bounded Three-Dimensional Turbulent Boundary Layers-Reference-Cited by-同舟云学术

Cross Flows in Bounded Three-Dimensional Turbulent Boundary Layers

Published:1973-08 Issue:4 Volume:15 Page:274-284
ISSN:0022-2542
Container-title:Journal of Mechanical Engineering Science
language:en
Short-container-title:Journal of Mechanical Engineering Science

Author:

Horlock J. H.¹

Affiliation:

1. S.R.C. Turbomachinery Laboratory, University Engineering Department, Madingley Road, Cambridge. Fellow of the Institution

Abstract

A study is made of the flow normal to the mainstream direction (cross flow) that takes place in three-dimensional ‘bounded’ turbulent boundary layers near a wall, i.e. boundary layers restricted by the presence of bounding surfaces normal to that wall. Such boundary layers are present in the flow through rows of blades in a turbo machine. Analytical expressions for the cross-flow velocity profiles are derived for these ‘bounded’ boundary layers and are compared with experimental data.

Publisher

SAGE Publications

Subject

General Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/JMES_JOUR_1973_015_049_02

Reference25 articles.

1. Boundary layers in three dimensions

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Secondary Flow in Repeating Stages of Axial Turbomachines;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;1995-05

2. Methode zur Berechnung von Randzonenkorrekturen in mehrstufigen axialen Turbomaschinen;Forschung im Ingenieurwesen;1991-03

3. Computation of Turbomachinery Boundary Layers;Aerothermodynamics of Aircraft Engine Components;1985-01

4. Wall Boundary Layer Development Near the Tip Region of an IGV of an Axial Flow Compressor;Journal of Engineering for Gas Turbines and Power;1984-04-01

5. Characteristics of the flow in the annulus-wall region of an axial-flow compressor rotor blade passage;20th Aerospace Sciences Meeting;1982-01-11