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An algebraic transition model combined with the k-ω RANS model for turbomachinery use

Slawomir Kubacki and Erik Dick (UGent)
(2016) ERCOFTAC BULLETIN. 2016(106). p.60-65
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Abstract
The functioning of a recently developed algebraic model for laminar to turbulent boundary layer transition under high free-stream turbulence is illustrated. The model uses only local variables and is tuned for turbomachinery flows. The transition model is combined with the newest k-omega RANS turbulence model by Wilcox. It takes into account two effects in an attached pre-transitional boundary layer: damping of short-wavelength disturbances induced by the free stream and breakdown of the near-wall perturbed flow with generation of fine-scale turbulence.
Keywords
turbomachinery, laminar-to-turbulent transition

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MLA
Kubacki, Slawomir, and Erik Dick. “An Algebraic Transition Model Combined with the K-ω RANS Model for Turbomachinery Use.” ERCOFTAC BULLETIN, vol. 2016, no. 106, 2016, pp. 60–65.
APA
Kubacki, S., & Dick, E. (2016). An algebraic transition model combined with the k-ω RANS model for turbomachinery use. ERCOFTAC BULLETIN, 2016(106), 60–65.
Chicago author-date
Kubacki, Slawomir, and Erik Dick. 2016. “An Algebraic Transition Model Combined with the K-ω RANS Model for Turbomachinery Use.” ERCOFTAC BULLETIN 2016 (106): 60–65.
Chicago author-date (all authors)
Kubacki, Slawomir, and Erik Dick. 2016. “An Algebraic Transition Model Combined with the K-ω RANS Model for Turbomachinery Use.” ERCOFTAC BULLETIN 2016 (106): 60–65.
Vancouver
1.
Kubacki S, Dick E. An algebraic transition model combined with the k-ω RANS model for turbomachinery use. ERCOFTAC BULLETIN. 2016;2016(106):60–5.
IEEE
[1]
S. Kubacki and E. Dick, “An algebraic transition model combined with the k-ω RANS model for turbomachinery use,” ERCOFTAC BULLETIN, vol. 2016, no. 106, pp. 60–65, 2016.
@article{7184667,
  abstract     = {{The functioning of a recently developed algebraic model for laminar to turbulent boundary layer transition under high free-stream turbulence is illustrated. The model uses only local variables and is tuned for turbomachinery flows. The transition model is combined with the newest k-omega RANS turbulence model by Wilcox. It takes into account two effects in an attached pre-transitional boundary layer: damping of short-wavelength disturbances induced by the free stream and breakdown of the near-wall perturbed flow with generation of fine-scale turbulence.}},
  author       = {{Kubacki, Slawomir and Dick, Erik}},
  issn         = {{2518-0991}},
  journal      = {{ERCOFTAC BULLETIN}},
  keywords     = {{turbomachinery,laminar-to-turbulent transition}},
  language     = {{eng}},
  number       = {{106}},
  pages        = {{60--65}},
  title        = {{An algebraic transition model combined with the k-ω RANS model for turbomachinery use}},
  url          = {{https://www.ercoftac.org/publications/ercoftac_bulletin/bulletin_106/}},
  volume       = {{2016}},
  year         = {{2016}},
}