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contributor authorA. Arnone
contributor authorR. Pacciani
date accessioned2017-05-08T23:51:50Z
date available2017-05-08T23:51:50Z
date copyrightOctober, 1996
date issued1996
identifier issn0889-504X
identifier otherJOTUEI-28655#679_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117796
description abstractA 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleRotor-Stator Interaction Analysis Using the Navier–Stokes Equations and a Multigrid Method
typeJournal Paper
journal volume118
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2840923
journal fristpage679
journal lastpage689
identifier eissn1528-8900
keywordsNavier-Stokes equations
keywordsRotors
keywordsStators
keywordsBlades
keywordsSteady state
keywordsGas turbines
keywordsStability AND Spacetime
treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 004
contenttypeFulltext


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