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Numerical Heat Transfer Part A: Applications, Vol. 66, Iss. 12, 2014-12 ,pp. : 1341-1364

Taylor & Francis Ltd

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Reynolds Stress Transport Modeling of Film Cooling at the Leading Edge of a Symmetrical Turbine Blade Model

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Heat Transfer Engineering, Vol. 29, Iss. 11, 2008-11 ,pp. : 950-960

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Measurement of Film Effectiveness for Cylindrical and Row Trenched Cooling Holes at Different Blowing Ratios

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Turbulence intensity effects on film cooling and heat transfer from compound angle holes with particular application to gas turbine blades

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Effect of turbine-blade cooling on the HAT (humid air turbine) cycle

By Gallo W.L.R.   Bidini G.   Bettagli N.   Facchini B.  

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