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Prediction of bypass and separation-induced transition with an algebraic intermittency model

Slawomir Kubacki, Tomasz Borzecki and Erik Dick (UGent)
(2016) ERCOFTAC BULLETIN. 108. p.48-53
Author
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Abstract
The paper discusses an algebraic intermittency model for prediction of bypass and separation-induced boundary layer transition. The transition model is coupled with a k-omega turbulence model. The transition model uses only local variables and is tuned for turbomachinery flows. For bypass transition, two effects in an attached pre-transitional boundary layer are modelled: damping of small-scale disturbances induced by the free stream and breakdown of the near-wall perturbed flow with generation of fine-scale turbulence. For separated flow, the model describes breakdown of a laminar free shear layer.
Keywords
turbomachinery flows, transition model

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MLA
Kubacki, Slawomir, et al. “Prediction of Bypass and Separation-Induced Transition with an Algebraic Intermittency Model.” ERCOFTAC BULLETIN, edited by M. Marek, vol. 108, Czestochowa University of Technology, 2016, pp. 48–53.
APA
Kubacki, S., Borzecki, T., & Dick, E. (2016). Prediction of bypass and separation-induced transition with an algebraic intermittency model. ERCOFTAC BULLETIN, 108, 48–53.
Chicago author-date
Kubacki, Slawomir, Tomasz Borzecki, and Erik Dick. 2016. “Prediction of Bypass and Separation-Induced Transition with an Algebraic Intermittency Model.” Edited by M. Marek. ERCOFTAC BULLETIN 108: 48–53.
Chicago author-date (all authors)
Kubacki, Slawomir, Tomasz Borzecki, and Erik Dick. 2016. “Prediction of Bypass and Separation-Induced Transition with an Algebraic Intermittency Model.” Ed by. M. Marek. ERCOFTAC BULLETIN 108: 48–53.
Vancouver
1.
Kubacki S, Borzecki T, Dick E. Prediction of bypass and separation-induced transition with an algebraic intermittency model. Marek M, editor. ERCOFTAC BULLETIN. 2016;108:48–53.
IEEE
[1]
S. Kubacki, T. Borzecki, and E. Dick, “Prediction of bypass and separation-induced transition with an algebraic intermittency model,” ERCOFTAC BULLETIN, vol. 108, pp. 48–53, 2016.
@article{8173652,
  abstract     = {{The paper discusses an algebraic intermittency model for prediction of bypass and separation-induced boundary layer transition. The transition model is coupled with a k-omega turbulence model. The transition model uses only local variables and is tuned for turbomachinery flows. For bypass transition, two effects in an attached pre-transitional boundary layer are modelled: damping of small-scale disturbances induced by the free stream and breakdown of the near-wall perturbed flow with generation of fine-scale turbulence. For separated flow, the model describes breakdown of a laminar free shear layer.}},
  author       = {{Kubacki, Slawomir and Borzecki, Tomasz and Dick, Erik}},
  editor       = {{Marek, M.}},
  issn         = {{2518-0991}},
  journal      = {{ERCOFTAC BULLETIN}},
  keywords     = {{turbomachinery flows,transition model}},
  language     = {{eng}},
  pages        = {{48--53}},
  publisher    = {{Czestochowa University of Technology}},
  title        = {{Prediction of bypass and separation-induced transition with an algebraic intermittency model}},
  volume       = {{108}},
  year         = {{2016}},
}