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An Investigation of the Flow in Manifolds with Open and Closed Ends

Published online by Cambridge University Press:  28 July 2016

J. H. Horlock
J. H. Horlock*
Affiliation:
Engineering Department, Massachusetts Institute of Technology
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Extract

The possibility of control of circulation around aircraft wings and gas turbine blades by ejection of air from the aerofoil into the main stream has drawn attention to the manifold problem. Discharge velocity distributions along the length of the wing or blade must be uniform, and it is important that the detailed nature of the flow in the supply manifolds should be understood. The distributions of velocity in manifolds supplying multicylinder internal combustion engines, in gas burners and in manifolds supplying canal locks are other allied problems.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 551 , November 1956 , pp. 749 - 753
Copyright
Copyright © Royal Aeronautical Society 1956

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References

1. Davidson, I. M. (1956). The Jet Flap. Journal of the Royal Aeronautical Society, p. 25, January 1956.CrossRefGoogle Scholar
2. Keller, J. D. (1949). The Manifold Problem. Transactions of the American Society of Mechanical Engineers, Vol. 71, 1949.Google Scholar
3. Allen, J. and Albinson, B. (1955). An Investigation of the Manifold Problem for Incompressible Fluids with Special Reference to the Use of Manifolds for Canal Locks. Proceedings of the Institution of Civil Engineers, Vol. 4, April 1955.Google Scholar
4. Dow, W. M. (1950). The Uniform Distribution of a Fluid Flowing Through a Perforated Pipe. Transactions of the American Society of Mechanical Engineers, Vol. 72, 1950.Google Scholar
5. Peirce, B. O. (1929). A Short Table of Integrals. Ginn and Company, p. 11, 1929.Google Scholar