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The solution of three-variable duct-flow equationsThis paper establishes a numerical method for the solution of three-variable problems and is applied here to rotational flows through ducts of various cross sections. An iterative scheme is developed, the main feature of which is the addition of a duplicate variable to the forward component of velocity. Two forward components of velocity result from integrating two sets of first order ordinary differential equations for the streamline curvatures, in intersecting directions across the duct. Two pseudo-continuity equations are introduced with source/sink terms, whose strengths are dependent on the difference between the forward components of velocity. When convergence is obtained, the two forward components of velocity are identical, the source/sink terms are zero, and the original equations are satisfied. A computer program solves the exact equations and boundary conditions numerically. The method is economical and compares successfully with experiments on bent ducts of circular and rectangular cross section where secondary flows are caused by gradients of total pressure upstream.
Document ID
19750003108
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stuart, A. R.
(Aston Univ. Birmingham, United Kingdom)
Hetherington, R.
(Rolls-Royce Ltd.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Publication Information
Publication: Pennsylvania State Univ. Fluid Mech., Acoustics, and Design of Turbomachinery, Pt. 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
75N11180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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