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Thole K.(1998)Flowfield Measurements for Film-Cooling Holes with Expanded Exits ASME, J. Turbomachinery 120 327-336
[2]
Gritsch M.(1998)Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes with Expanded Exits ASME, J. Turbomachinery 120 549-556
[3]
Schulz A.(2001)Film Cooling Predictions of Simple and Compound Angle Injection from One and Two Staggered Rows Numer. Heat Transfer, Part A 40 273-294
[4]
Wittig S.(2001)Effect of Compound Angle Injection on Flat Surface Film Cooling with Large Streamwise Injection Angle Experiment. Thermal Fluid Sci. 25 23-29
[5]
Gritsch M.(2003)Improved Film Cooling from Cylindrical Angled Holes with Triangular Tabs: Effect of Tab Orientations Int. J. Heat Fluid Flow 24 657-668
[6]
Schulz A.(1996)Film Cooling with Compound Angle Holes: Adiabatic Effectiveness ASME, J. Turbomachinery 118 807-813
[7]
Wittig S.(2002)Film Cooling Effectiveness and Heat Transfer Coefficient Distributions Around Diffusion Shaped Holes Trans. ASME, J. Heat Transfer 124 820-827
[8]
Azzi A.(1997)The Effect of Vortex Generators on a Jet in a Crossflow Phys. Fluids 9 106-114
[9]
Abidat M.(1985)Effect of Surface Roughness on Film Cooling Performance ASME, J. Eng. Gas Turbines Power 107 111-116
[10]
Jubran B. A.(2013)Film Cooling of Cylindrical Hole with a Downstream Short Crescent-Shaped Block ASME Paper 135 031702-1605