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E. , “Redesigned 26-Inch Last Stage for Improved Turbine Reliability and Efficiency,” ASME Paper No. 84-JPGC-GT17, 1984. (Also published as GE Power Generation Turbine Technology Reference Library Paper No. G. , “An Update on Steam Turbine Redesigns for Improved Efficiency and Availability,” GE Power Generation Turbine Technology Reference Librar y Paper No. GER-3577, 1988. , “Steam Turbine Long Bucket Developments,” GE Power Generation Turbine Technology Reference Librar y Paper GER-3647, 1990.

The Bezier curve representation allows individual parameters to be varied without requiring fine tuning of the other parameters to achieve reasonable shapes. The program is coupled to a fast 2D flow solver that allows the designer to manipulate the blade shape and receive quick feedback on the effect of the shape change on the blade sur face Mach number distribution. Individual blade cross-sections can be radially stacked to form a complete blade, and curves diminish, leading to substantial reductions in development cycle time and cost and more efficient, reliable turbine designs.

11. 12. REFERENCES 1. 2. 3. 4. , “Crossflows in a Turbine Cascade Passage,” ASME Jour nal of Engineering for Power, Vol. 102, No. 4, October, 1980, pp. 866-874. G. , “A ThreeDimensional Euler Solver for Turbomachiner y Blade Rows,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, April, 1985, pp. 258264. G. , “An Investigation of Turbulence Modeling in Transonic Fans Including a Novel Implementation of an Implicit k-e Turbulence Model,” ASME Paper 92-GT308, 1992. P. , “The Use of Orthogonal 13.

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