Three-dimensional calculations of the flow field around a turbine blade with film cooling injection near the leading edge

DOI10.1023/A:1011437523546zbMath1076.76041OpenAlexW2170048181MaRDI QIDQ5952018

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Publication date: 2001

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1011437523546

zbMATH Keywords

compressibility effectsSIMPLE algorithmaveraged Navier-Stokes equationsfinite volume multi-block solver

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General theory of rotating fluids (76U05) Compressibility effects in turbulence (76F50)

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Application of the TLVA model for predicting film cooling under rotating frames ⋮ Investigation of density ratio effects on normally injected cold jets into a hot cross flow

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