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RESEARCH PAPERS

A Variational Formulation of the Compressible Throughflow Problem

[+] Author and Article Information
G. C. Oates

Department of Aeronautics and Astronautics, University of Washington, Seattle, Wa.

C. J. Knight

Avco-Everett Research Laboratory, Inc., Everett, Mass.

G. F. Carey

Aerospace Research Laboratory, University of Washington, Seattle, Wa.

J. Eng. Power 98(1), 1-8 (Jan 01, 1976) (8 pages) doi:10.1115/1.3446105 History: Received December 02, 1974; Online July 14, 2010

Abstract

A variational formulation of the compressible throughflow problem is developed. The method is suitable for the calculation of throughflow flow fields in which large rotational effects, large compressibility effects and large variations in hub and tip radii may exist. The formulation requires the absence of viscous forces between the blade rows, though the effects of losses within the blade rows may be included through the variation of entropy across stream surfaces. The meridional Mach number is restricted to be less than unity, though the complete flow Mach number may be much in excess of unity. The variational formulation represents a complete statement of the problem in that the boundary conditions, far upstream and far downstream conditions, and matching conditions at all actuator disks are all natural conditions of the variational formulation. Furthermore, terms involving density variations vanish. The variational problem is posed in terms of the streamline position and the density. A finite element approximation produces a coupled nonlinear algebraic problem for numerical solution. Example calculations of flows with highly-loaded actuator disks, existing in annuli with large variations in hub and tip radii, are given.

Copyright © 1976 by ASME
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