An interactive optimization procedure applied to the design of gas turbine discs
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Abstract An interactive procedure based on the Complex method is applied to the design of a minimum weight gas turbine air-cooled disc. The disc profile is defined by spline interpolation and an interactive video display terminal is used to show the results of the thermal and stress analyses at each step of the optimization. The advantages of interactivity are shown in a practical example.
[1] Albert D. M. Lewis,et al. Computer-augmented preliminary design of aircraft wing structures☆ , 1976 .
[2] M. J. Box. A New Method of Constrained Optimization and a Comparison With Other Methods , 1965, Comput. J..
[3] B. M. E. de Silva. Minimum Weight Design of Disks Using a Frequency Constraint , 1969 .
[4] A. J. Morris,et al. A review of techniques for automated structural design , 1977 .