A recently developed, time-accurate multigrid viscous 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. By means of a dual time-stepping approach, 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. The accelerating strategies include local time stepping, residual smoothing, and multigrid. Two-dimensional viscous calculations of unsteady rotor-stator interaction in the first stage of a modern gas turbine are presented. The stage analysis is based on the introduction of several blade passages to approximate the stator:rotor count ratio. Particular attention is dedicated to grid dependency in space and time as well as to the influence of the number of blades included in the calculations.

Rotor-Stator Interaction Analysis Using the Navier-Stokes Equations and a Multigrid Method / Andrea Arnone; Roberto Pacciani. - STAMPA. - ASME paper 95-GT-177:(1995), pp. 1-15. (Intervento presentato al convegno International Gas Turbine and Aeroengine Congress and Exposition tenutosi a Houston, TX, USA nel 5 June 1995 through 8 June 1995).

Rotor-Stator Interaction Analysis Using the Navier-Stokes Equations and a Multigrid Method

ARNONE, ANDREA;PACCIANI, ROBERTO
1995

Abstract

A recently developed, time-accurate multigrid viscous 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. By means of a dual time-stepping approach, 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. The accelerating strategies include local time stepping, residual smoothing, and multigrid. Two-dimensional viscous calculations of unsteady rotor-stator interaction in the first stage of a modern gas turbine are presented. The stage analysis is based on the introduction of several blade passages to approximate the stator:rotor count ratio. Particular attention is dedicated to grid dependency in space and time as well as to the influence of the number of blades included in the calculations.
1995
Conference Proceedings
International Gas Turbine and Aeroengine Congress and Exposition
Houston, TX, USA
5 June 1995 through 8 June 1995
Andrea Arnone; Roberto Pacciani
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/877320
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