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Numerical modeling of gas flow around oscillating compressor blades

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Abstract

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.

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Authors
  1. S. V. Rusakov
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  2. N. V. Shuvaev
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Additional information

Original Russian Text © S.V. Rusakov, N.V. Shuvaev, 2011, published in Vychislitel’naya Mekhanika Sploshnykh Sred, 2011, Vol. 4, No. 1, pp. 101–108.

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Rusakov, S.V., Shuvaev, N.V. Numerical modeling of gas flow around oscillating compressor blades. Fluid Dyn 46, 665–671 (2011). https://doi.org/10.1134/S0015462811040168

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  • DOI: https://doi.org/10.1134/S0015462811040168

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