Working range optimization for turbine and compressor blading
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摘要
A partially reduced SQP algorithm for a multiple setpoint industrial design optimization problem is presented. It is highlighted that the modularity of this concept has made it possible to apply it to problems as complex as working range optimization in high-temperature gas turbine and compressor blade design. Further emphasis is drawn on parallelization aspects and practical experiences in engineering practice.
论文关键词：Multiple setpoint optimization,Partially reduced SQP methods,Shape optimization,Transonic cascade flow,Turbine and compressor S1-streamsurface blade design
论文评审过程：Received 22 January 1998, Revised 20 December 1999, Available online 18 July 2000.
论文官网地址：https://doi.org/10.1016/S0377-0427(00)00303-4
