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The Design of an Annular Entry to a Circular Duct

Published online by Cambridge University Press:  07 June 2016

J. C. Gibbings
J. C. Gibbings*
Affiliation:
Department of Fluid Mechanics, University of Liverpool
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Extract

This report describes the design of an annular entry for the axisymmetric flow into a circular duct, shaped so that the wall velocity gradients are favourable to the development of the boundary layer flow. As a first step the accelerating flow around a two-dimensional 90° duct bend with favourable gradients was obtained. This shape was modified and the axisymmetric flow pattern through it obtained by a combination of electrical analogue and relaxation methods and then checked by experiment. The favourable gradients were retained in the axisymmetric flow.

Type
Research Article
Information
Aeronautical Quarterly , Volume 10 , Issue 4 , November 1959 , pp. 361 - 372
Copyright
Copyright © Royal Aeronautical Society. 1959

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References

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