Investigation of flow in the crowns of compressors using different turbulence models
DOI:
https://doi.org/10.15587/1729-4061.2011.2445Keywords:
Aerodynamics in compressors, computational fluid dynamicsAbstract
The results of flow modelling in Rotor37compressor blade row using k-ω и SST turbulence models are presented. The analysis of applicability of turbulence models for prediction of compressor row aerodynamic characteristics, based on modeling results, is performedReferences
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Copyright (c) 2014 Юрий Адольфович Быков
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