Abstract
This paper describes a new computational tool developed for the analysis of two or three dimensional, viscous or inviscid turbomachinery flutter and forced response problems. Time harmonic results are obtained by linearizing the underlying steady flow numerical algorithm, including the k-ω turbulence model. Solutions are obtained via explicit time marching, with multigrid, on multiblock grids. We present results that focus on the role of the linearization of the viscous terms and the turbulence model in the accurate computation of linearized unsteady flows.
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Holmes, D.G., Lorence, C.B. (1998). Three Dimensional Linearized Navier-Stokes Calculations for Flutter and Forced Response. In: Fransson, T.H. (eds) Unsteady Aerodynamics and Aeroelasticity of Turbomachines. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-5040-8_14
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DOI: https://doi.org/10.1007/978-94-011-5040-8_14
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-6116-2
Online ISBN: 978-94-011-5040-8
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