Marek Soliński
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Publication showcase
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The Unsteady Low-Frequency Forces Acting on the Rotor Blade in the First Stage on an Axial Compressor of SO-3 Jet Engine
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Dynamic analysis of the first stage compressor bladed disc of an aircraft engine
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Influence of mesh density on 2D viscous flutter in a turbomachinery cascade
In this study numerical simulations of 2D viscous flutter were performed and compared with available experimental results for various mesh densities and flow parameters. Calculations were carried out for the bending oscillations of an Eleventh Standard Configuration cascade. ANSYS CFX code was used for the SST, SA and k-ω turbulence model calculations.
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