2023
DOI: 10.1115/1.4056407
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A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation

Abstract: This paper describes a framework to quantify the effect of freestream turbulence, generated by mixing processes in a combustor, on turbulent boundary layer loss generation in the high pressure turbine downstream of the combustor. The regime of freestream turbulence common to gas turbine aero engines is identified and it is shown that the dissipation loss coefficient in this regime can be determined using existing measurements of the effect of freestream turbulence on skin friction. The paper shows that combust… Show more

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