Title of article
Working range optimization for turbine and compressor blading
Author/Authors
Egartner، نويسنده , , Wolfgang، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2000
Pages
7
From page
59
To page
65
Abstract
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.
Keywords
Partially reduced SQP methods , Transonic cascade flow , Turbine and compressor S1-streamsurface blade design , Shape optimization , Multiple setpoint optimization
Journal title
Journal of Computational and Applied Mathematics
Serial Year
2000
Journal title
Journal of Computational and Applied Mathematics
Record number
1551136
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