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Numerical Simulation of 3D Viscous Flow in a Linear Compressor Cascade With Tip Clearance PUBLIC ACCESS

[+] Author Affiliations
Shun Kang, Charles Hirsch

Vrije Universiteit Brussel, Brussel, Belgium

Paper No. 94-GT-364, pp. V001T01A125; 13 pages
doi:10.1115/94-GT-364
From:
  • ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • The Hague, Netherlands, June 13–16, 1994
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7883-5
  • Copyright © 1994 by ASME

abstract

A Navier-Stokes solver is applied to investigate the 3D viscous flow in a low speed linear compressor cascade with tip clearance at design and off-design conditions with two different meshes. The algebraic turbulence model of Baldwin-Lomax is used for closure. Relative motion between the blades and wall is simulated for one flow coefficient. Comparisons with experimental data, including flow structure, static and total pressures, velocity profiles, secondary flows and vorticity, are presented for the stationary wall case. It is shown that the code predicts well the flow structure observed in experiments and shows the details of the tip leakage flow and the leading edge horseshoe vortex.

Copyright © 1994 by ASME
This article is only available in the PDF format.

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