Abstract
Turbulence plays an important role in the flow physics through the high pressure turbine (HPT), yet its evolution through the stage is still poorly understood. Furthermore, achieving high values, on the order of 10–20%, can be both challenging and costly in an experimental facility. Numerous experimental efforts have been undertaken to mimic the turbulence levels exiting a combustor.
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Kopriva, J.E., Laskowski, G.M., Sheikhi, M.R.H. (2018). Hybrid LES of a High Pressure Turbine Nozzle/Blade Interaction. 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_34
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DOI: https://doi.org/10.1007/978-3-319-63212-4_34
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