Abstract
The improvement of centrifugal compressor performance and the control of the radial forces acting on the impeller due to the circumferential variation of the static pressure caused by the volute require a good understanding of the flow mechanisms and an accurate prediction of the flow pattern inside the volute. A 3D volute calculation method has been developed for this purpose. The volute is discretized by means of hexahedral elements. A cell vertex finite volume approach is used in combination with a time marching procedure. The numerical procedure makes use of a central space discretization and a four step Runge-Kutta time stepping scheme. The artificial dissipation used in the solver is based on the fourth order differences of the conservative variables. Implicit residual smoothing improves the convergence rate. The loss model implemehted in the code accounts for the losses due to internal shear and friction losses on the walls. A comparison of the calculated and measured results inside a volute with elliptical cross sectional shape reveals that the modified Euler solver accurately predicts the velocity and pressure distribution inside and upstream of the volute.
Original language | English |
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Title of host publication | Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery |
Publisher | American Society of Mechanical Engineers |
ISBN (Electronic) | 9780791878880 |
DOIs | |
Publication status | Published - 1993 |
Externally published | Yes |
Event | ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 - Cincinnati, United States Duration: 24 May 1993 → 27 May 1993 |
Publication series
Name | ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 |
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Volume | 1 |
Conference
Conference | ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993 |
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Country/Territory | United States |
City | Cincinnati |
Period | 24/05/93 → 27/05/93 |
Bibliographical note
Publisher Copyright:Copyright © 1993 by ASME.