A Navier-Stokes time-accurate solver has been extended to the analysis of unsteady rotor-stator interaction. In the proposed method, a fully-implicit time discretization is used to remove stability limitations. A four-stage Runge-Kutta scheme is used in conjunction with several accelerating techniques typical of steady-state solvers, instead of traditional time-expensive factorizations. Those accelerating strategies include local time stepping, residual smoothing, and multigrid. Direct interpolation of the conservative variables is used to handle the interfaces between blade rows. Two-dimensional viscous calculations of unsteady rotor-stator interaction in a modern gas turbine stage are presented to check for the capability of the procedure.
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December 1995
Research Papers
Multigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations
A. Arnone,
A. Arnone
Department of Energy Engineering, University of Florence, Via S. Marta, 3, 50139 Florence, Italy
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R. Pacciani,
R. Pacciani
Institute of Energetics, University of Perugia, Perugia, Italy
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A. Sestini
A. Sestini
Department of Energy Engineering, University of Florence, Florence, Italy
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A. Arnone
Department of Energy Engineering, University of Florence, Via S. Marta, 3, 50139 Florence, Italy
R. Pacciani
Institute of Energetics, University of Perugia, Perugia, Italy
A. Sestini
Department of Energy Engineering, University of Florence, Florence, Italy
J. Fluids Eng. Dec 1995, 117(4): 647-652 (6 pages)
Published Online: December 1, 1995
Article history
Received:
April 20, 1994
Revised:
February 17, 1995
Online:
December 4, 2007
Citation
Arnone, A., Pacciani, R., and Sestini, A. (December 1, 1995). "Multigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations." ASME. J. Fluids Eng. December 1995; 117(4): 647–652. https://doi.org/10.1115/1.2817317
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