A finite element overlapping scheme for turbomachinery flows on parallel platforms-Reference-Cited by-同舟云学术

A finite element overlapping scheme for turbomachinery flows on parallel platforms

Published:2003-08 Issue:7 Volume:32 Page:1017-1047
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Borello D.,Corsini A.,Rispoli F.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference52 articles.

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3. The role of tip leakage vortex breakdown in compressor rotor aerodynamics;Furukawa;J. Turbomach.,1999

4. Eulitz F. Numerical simulation and modeling of unsteady turbomachinery flows. In: Recent developments in numerical methods for turbomachinery flows. VKI LS 2002-01

5. Development of hub corner stall and its influence on the performance of axial compressor blade rows;Hah;J. Turbomach.,1999

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