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Numerical Computation of Unsteady Flows at Low Frequencies in the Last Stage of a Steam Turbine FREE

[+] Author Affiliations
R. Lattermann, J. Wachter

Universität Stuttgart, West Germany

Paper No. 87-GT-143, pp. V001T01A039; 8 pages
doi:10.1115/87-GT-143
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 1: Turbomachinery
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7923-8
  • Copyright © 1987 by ASME

abstract

The asymmetric flow field downstream the final stage of steamturbines causes an unsteady aerodynamic loading of the rotor in the range of the lower blade eigenfrequencies. A numerical solution for the time-dependent Euler equations is presented for a complete turbine stage, varying the outlet pressure sinusoidally in the rotating frame of reference. A two-dimensional blade-to-blade flow model is used including variable streamsheet thickness and changing radii. The equations are solved by an explicit time-marching finite difference algorithm of second order accuracy in space and time. Additionally the quasi-steady solution is compared with measurements in a model steam turbine.

Copyright © 1987 by ASME
This article is only available in the PDF format.

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