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Jackson, Dale Jay | Aerodynamic mixing losses and discharge coefficients due to film cooling from a symmetric turbine airfoil in transonic flow | Aerodynamic losses and discharge coefficients are obtained for two different Pratt and Whitney axisymetric turbine airfoils with film cooling holes. Blade 3 results are given for the blowing ratios, of 0.42, 0.73, and 1.28. The pressure ratios are 1.18, 1.45, and 2.07 for the "ambient" tests and 1.1... | Mechanical Engineering | 1998-12 |
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