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contributor authorA. Arnone
contributor authorR. Pacciani
contributor authorA. Sestini
date accessioned2017-05-08T23:47:27Z
date available2017-05-08T23:47:27Z
date copyrightDecember, 1995
date issued1995
identifier issn0098-2202
identifier otherJFEGA4-27099#647_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115461
description abstractA 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleMultigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations
typeJournal Paper
journal volume117
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2817317
journal fristpage647
journal lastpage652
identifier eissn1528-901X
keywordsNavier-Stokes equations
keywordsRotors
keywordsComputation
keywordsStators
keywordsSteady state
keywordsInterpolation
keywordsBlades
keywordsGas turbines AND Stability
treeJournal of Fluids Engineering:;1995:;volume( 117 ):;issue: 004
contenttypeFulltext


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