2004
DOI: 10.1002/zamm.200310087
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2D shape optimization of turbine blades

Abstract: In this paper, we present methods to optimize the efficiency of turbine blades. The profile of a turbine blade is parameterized by curves, its parameters form the variables of a nonlinear optimization problem. Because of the very expensive function evaluation, gradient based optimization methods are preferred. In order to provide gradient information for the optimization method, the fluid sensitivities have to be considered. Theoretical properties and implementation aspects for the sensitivity equation are dis… Show more

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Cited by 2 publications
(4 citation statements)
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“…Montrone et al . and Morris et al . presented 2D shape parameterization methods that can be used to optimize the turbine blade profile.…”
Section: Introductionmentioning
confidence: 89%
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“…Montrone et al . and Morris et al . presented 2D shape parameterization methods that can be used to optimize the turbine blade profile.…”
Section: Introductionmentioning
confidence: 89%
“…Starzmann [25] and Starzmann and Carolus [26] designed the Wells turbine blade using a code based on the classical blade element approach. Montrone et al [27] and Morris et al [28] presented 2D shape parameterization methods that can be used to optimize the turbine blade profile. Grasso [29] optimized the airfoil of a tidal turbine by coupling a gradient-based algorithm with the RFOIL solver and a composite Bezier geometrical parameterization.…”
Section: Introductionmentioning
confidence: 99%
“…The most efficient method for providing gradient information for a large number of parameters is the adjoint method. It is discussed by Elliot [6], Giles et al [10], Iollo et al [17], and Jameson [19].The geometry optimization method in this paper, in its 2D aspects, is based upon [27] and [1]. Physical and technological aspects are discussed in [23,24].…”
mentioning
confidence: 99%
“…The geometry optimization method in this paper, in its 2D aspects, is based upon [27] and [1]. Physical and technological aspects are discussed in [23,24].…”
mentioning
confidence: 99%