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Transonic Cascade Flow Prediction Using the Navier-Stokes Equations PUBLIC ACCESS

[+] Author Affiliations
A. Arnone, S. S. Stecco

University of Florence, Florence, Italy

Paper No. 91-GT-313, pp. V001T01A096; 8 pages
doi:10.1115/91-GT-313
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7898-9
  • Copyright © 1991 by ASME

abstract

This paper presents results which summarize the work carried out during the last three years to improve the efficiency and accuracy of numerical predictions in turbomachinery flow calculations.

A new kind of non-periodic C-type grid is presented and a Runge-Kutta scheme with accelerating strategies is used as a flow solver.

The code capability is presented by testing four different blades at different exit Mach numbers in transonic regimes. Comparison with experiments shows the very good reliability of the numerical prediction. In particular the loss coefficient seems to be correctly predicted by using the well-known Baldwin-Lomax turbulence model.

Copyright © 1991 by ASME
This article is only available in the PDF format.

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