Abstract
On turbine blades, film cooling is an efficient way to prevent temperature to reach the blade material melting point, downstream the combustion chamber. Protection against continuous feeding of incoming hot gases is achieved by injecting coolant at the blade surface. To study turbulent mixing occurring in the jet vicinity we focus our attention on a jet in crossflow configuration.
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Acknowledgements
Authors are grateful for the computational resources that were provided by (i) CNRS on the BlueGene/Q system Turing, through the GENCI-IDRIS grants x20142a7178 and x20152a7178 and (ii) CALMIP on the Eos system through the p1425 allocation.
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Folkersma, M., Bodart, J. (2018). Large Eddy Simulation of an Asymmetric Jet in Crossflow. In: Grigoriadis, D., Geurts, B., Kuerten, H., Fröhlich, J., Armenio, V. (eds) Direct and Large-Eddy Simulation X. ERCOFTAC Series, vol 24. Springer, Cham. https://doi.org/10.1007/978-3-319-63212-4_10
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DOI: https://doi.org/10.1007/978-3-319-63212-4_10
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