Numerical modeling of gas flow around oscillating compressor blades

Numerical modeling of gas flow around oscillating compressor blades

The problem of gas flow around a plane cascade of oscillating blades is numerically solved using the ANSYS CFX package. The blade surface displacement is taken into account using a movable grid generated before the beginning of the calculations at each time step. The calculated and experimental data...

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Veröffentlicht in:Fluid dynamics 2011-08, Vol.46 (4), p.665-671
Hauptverfasser: Rusakov, S. V., Shuvaev, N. V.
Format: Artikel
Sprache:eng
Schlagworte:
Blades
Classical and Continuum Physics
Classical Mechanics
Compressor blades
Computational fluid dynamics
Engineering Fluid Dynamics
Fluid- and Aerodynamics
Gas flow
Mathematical models
Oscillating
Packages
Physics
Physics and Astronomy
Vibration
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container_title Fluid dynamics
container_volume 46
creator Rusakov, S. V.
Shuvaev, N. V.
description The problem of gas flow around a plane cascade of oscillating blades is numerically solved using the ANSYS CFX package. The blade surface displacement is taken into account using a movable grid generated before the beginning of the calculations at each time step. The calculated and experimental data are compared. The calculated results are used for determining the blade stability against flutter.
doi_str_mv 10.1134/S0015462811040168
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source SpringerNature Journals
subjects Blades
Classical and Continuum Physics
Classical Mechanics
Compressor blades
Computational fluid dynamics
Engineering Fluid Dynamics
Fluid- and Aerodynamics
Gas flow
Mathematical models
Oscillating
Packages
Physics
Physics and Astronomy
Vibration
title Numerical modeling of gas flow around oscillating compressor blades
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