An algebraic model for bypass transition in turbomachinery boundary layer flows
- Author
- Slawomir Kubacki and Erik Dick (UGent)
- Organization
- Keywords
- algebraic model, COMPRESSOR CASCADE, transition modelling, intermittency, bypass transition, turbomachinery, separated boundary layer, TURBINE BLADE, TURBULENCE, SIMULATIONS, DYNAMICS
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Citation
Please use this url to cite or link to this publication: http://hdl.handle.net/1854/LU-7094212
- MLA
- Kubacki, Slawomir, and Erik Dick. “An Algebraic Model for Bypass Transition in Turbomachinery Boundary Layer Flows.” INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, vol. 58, Elsevier, 2016, pp. 68–83, doi:10.1016/j.ijheatfluidflow.2016.01.001.
- APA
- Kubacki, S., & Dick, E. (2016). An algebraic model for bypass transition in turbomachinery boundary layer flows. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 58, 68–83. https://doi.org/10.1016/j.ijheatfluidflow.2016.01.001
- Chicago author-date
- Kubacki, Slawomir, and Erik Dick. 2016. “An Algebraic Model for Bypass Transition in Turbomachinery Boundary Layer Flows.” INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW 58: 68–83. https://doi.org/10.1016/j.ijheatfluidflow.2016.01.001.
- Chicago author-date (all authors)
- Kubacki, Slawomir, and Erik Dick. 2016. “An Algebraic Model for Bypass Transition in Turbomachinery Boundary Layer Flows.” INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW 58: 68–83. doi:10.1016/j.ijheatfluidflow.2016.01.001.
- Vancouver
- 1.Kubacki S, Dick E. An algebraic model for bypass transition in turbomachinery boundary layer flows. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW. 2016;58:68–83.
- IEEE
- [1]S. Kubacki and E. Dick, “An algebraic model for bypass transition in turbomachinery boundary layer flows,” INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, vol. 58, pp. 68–83, 2016.
@article{7094212,
author = {{Kubacki, Slawomir and Dick, Erik}},
issn = {{0142-727X}},
journal = {{INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW}},
keywords = {{algebraic model,COMPRESSOR CASCADE,transition modelling,intermittency,bypass transition,turbomachinery,separated boundary layer,TURBINE BLADE,TURBULENCE,SIMULATIONS,DYNAMICS}},
language = {{eng}},
pages = {{68--83}},
publisher = {{Elsevier}},
title = {{An algebraic model for bypass transition in turbomachinery boundary layer flows}},
url = {{http://doi.org/10.1016/j.ijheatfluidflow.2016.01.001}},
volume = {{58}},
year = {{2016}},
}
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