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LES of the Flow in a Rotating Rib-Roughened Duct

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Part of the book series: ERCOFTAC Series ((ERCO,volume 20))

Abstract

Interior channels of gas-turbine blades are often lined with ribs, which act as turbulence promoters to enhance heat transfer between the hot blade surface and the cooling air.

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References

  1. Coletti, F., Maurer, T., Arts, T., Di Sante, A.: Flow field investigation in a rotating rib-roughened channel by means of particle image velocimetry. Exp. Fluids 52, 1043–1061 (2012)

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  2. Delibra, G., Borello, D., Hanjalic, K., Rispoli, F.: LES of flow and heat transfer in a channel with a staggered cylindrical pin matrix. In: Armenio, V., Geurts, B., Froelich, J. (eds.) Direct and Large-Eddy Simulation VII, Proceedings of 7th International ERCOFTAC Workshop, Trieste. Springer Science and Media B.V., 9–10 Sept 2008

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  3. Casarsa, L., Arts, T.: Experimental investigation of the aerothermal performance of a high blockage rib-roughened cooling channel. J. Turbomach. 127, 580–588 (2005)

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Correspondence to D. Borello .

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© 2015 Springer International Publishing Switzerland

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Borello, D., Salvagni, A., Rispoli, F., Hanjalic, K. (2015). LES of the Flow in a Rotating Rib-Roughened Duct. In: Fröhlich, J., Kuerten, H., Geurts, B., Armenio, V. (eds) Direct and Large-Eddy Simulation IX. ERCOFTAC Series, vol 20. Springer, Cham. https://doi.org/10.1007/978-3-319-14448-1_35

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  • DOI: https://doi.org/10.1007/978-3-319-14448-1_35

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-14447-4

  • Online ISBN: 978-3-319-14448-1

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