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.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
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)
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
Casarsa, L., Arts, T.: Experimental investigation of the aerothermal performance of a high blockage rib-roughened cooling channel. J. Turbomach. 127, 580–588 (2005)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2015 Springer International Publishing Switzerland
About this paper
Cite this paper
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
Download citation
DOI: https://doi.org/10.1007/978-3-319-14448-1_35
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-14447-4
Online ISBN: 978-3-319-14448-1
eBook Packages: EngineeringEngineering (R0)