Experimental Investigation of the Laminar Flow Along a Straight 135° Corner-Reference-Cited by-同舟云学术

Experimental Investigation of the Laminar Flow Along a Straight 135° Corner

Published:1973-05 Issue:2 Volume:24 Page:147-154
ISSN:0001-9259
Container-title:Aeronautical Quarterly
language:en
Short-container-title:Aeronautical Quarterly

Author:

Barclay W H

Abstract

SummaryThe results of measurements in laminar flow along a straight 135° corner are presented. Near to the inlet edge plane the flow has an appearance resembling that reported by Zamir and Young for a 90° corner in which the isovels in transverse planes are concave outwards near the bisecting line of the corner, but unlike the 90° corner flow this characteristic diminishes with distance downstream in the case examined here. The analytical solution by Carrier is found to be a good representation of the flow in the 135° corner.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference11 articles.

1. On an equation occurring in Falkner and Skan's approximate treatment of the equations of the boundary layer

2. On the corner boundary layer with favourable pressure gradient;Zamir;Aeronautical Quarterly,1972

3. Incompressible flow along a corner

4. Viscous and resistive eddies near a sharp corner

5. The boundary layer in a corner

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