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Evaluation of an algebraic model for laminar-to-turbulent transition on secondary flow loss in a low-pressure turbine cascade with an endwall
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- Conference Paper
- C3
- open access
Transition models for turbomachinery boundary layer flows
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Prediction of endwall losses in a low pressure turbine cascade with an algebraic intermittency model
(2018) XXIII FLUID MECHANICS CONFERENCE (KKMP 2018). In Journal of Physics Conference Series 1101. p.116-117 -
An algebraic model for bypass transition in turbomachinery boundary layer flows
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An algebraic transition model combined with the k-ω RANS model for turbomachinery use