Surrogate Based Optimization Techniques for Aerodynamic Design of Turbomachinery

Abdus Samad, Kwang-Yong Kim

Research output: Contribution to specialist publicationLetter

Abstract

Recent development of high speed computers and use of optimization techniques have given a big momentum of turbomachinery design replacing expensive experimental cost as well as trial and error approaches. The surrogate based optimization techniques being used for aerodynamic turbomachinery designs coupled with Reynolds-averaged Navier-Stokes equations analysis involve single- and multi-objective optimization methods. The objectives commonly tried to improve were adiabatic efficiency, pressure ratio, weight etc. Presently coupling the fluid flow and structural analysis is being tried to find better design in terms of weight, flutter and vibration, and turbine life. The present article reviews the surrogate based optimization techniques used recently in turbomachinery shape optimizations.
Original languageEnglish
Pages179-188
Number of pages10
Volume2
No.2
Specialist publicationInternational Journal of Fluid Machinery and Systems
Publication statusPublished - Apr 2009

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Keywords

  • design engineering
  • fluid flow
  • fluids
  • mathematical analysis
  • Navier-Stokes equations
  • optimization
  • turbomachinery
  • vibration

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