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Compressible Shear Flows in the Duct with Varying Cross-Sectional Area

Published online by Cambridge University Press:  04 July 2016

S. Fujii
S. Fujii*
Affiliation:
National Aerospace Laboratory, Japan
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Summary:

The basic theory of the compressible non-swirling rotational flows through ducts with varying hub radii, associated with the concept of actuator discs, is described. The problem is simplified by considering a single-parameter in the radial velocity profile. Particular attention is given to the combined effects of the taper of inside walls and also of compressibility on the radial velocity and the axial velocity profile. The derived ordinary differential equation with non-homogeneous terms can be reduced to the well-known formula of classical actuator disc theories for the cylindrical passage. A numerical example is also presented.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 71 , Issue 674 , February 1967 , pp. 128 - 132
Copyright
Copyright © Royal Aeronautical Society 1967

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