Abstract
Based on an artificial compressibility method, the explicit Runge-Kutta time stepping finite difference algorithm was applied to steady, incompressible, Navier-Stokes equations. A two-dimensional analysis computer code in a generalized curvilinear coordinate system was developed and its accuracy has been compared to known numerical solutions. The algorithm has been accelerated using our new Distributed Minimal Residual (DMR) method, which allows each equation in the system to advance in time with its own optimal speed. The effectiveness of the DMR method was examined for a number of test cases. The accelerated algorithm offers substantial savings of the computing time.
Original language | English |
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Title of host publication | Turbomachinery |
Publisher | American Society of Mechanical Engineers (ASME) |
ISBN (Electronic) | 9780791879139 |
DOIs | |
State | Published - 1989 |
Externally published | Yes |
Event | ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition, GT 1989 - Toronto, Canada Duration: 4 Jun 1989 → 8 Jun 1989 |
Publication series
Name | Proceedings of the ASME Turbo Expo |
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Volume | 1 |
Conference
Conference | ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition, GT 1989 |
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Country/Territory | Canada |
City | Toronto |
Period | 4/06/89 → 8/06/89 |
Bibliographical note
Publisher Copyright:Copyright © 1989 by ASME.