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Title : PARALLEL THERMOELASTICITY OPTIMIZATION OF 3-D SERPENTINE COOLING PASSAGES IN TURBINE BLADES
Company : Sigma Technology
File Name : ASME2003-38180-new.pdf
Size : 333148
Type : application/pdf
Date : 17-Apr-2010
Downloads : 3

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An automatic design algorithm for parametric shape optimization of three-dimensional cooling passages inside axial gas turbine blades has been developed. A robust semi-stochastic constrained optimizer (IOSO) and a parallel genetic algorithm were used to solve this problem while running on an inexpensive distributed memory parallel computer.
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