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Study on aerodynamic optimization design of multistage axial turbine under multiple working conditions

  • Hong Lei Zhao*
  • , Song Tao Wang
  • , Wan Jin Han
  • , Guo Tai Feng
  • *Corresponding author for this work
  • School of Energy Science and Engineering, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

A three-stage axial turbine was redesigned by using an aerodynamic optimization design process of multistage axial turbine in multiple working conditions, which combines quasi-3D design methods and multistage local optimization methods. Genetic algorithm and artificial neural network were employed to 3D local optimization of various cascades. The flow field was computed through a three-dimensional viscosity Navier-Stokes equation. With optimization design, the performance of every cascade was optimized, and the overall efficiency increased by 1% under the reliable total flow mass, indicating that the total performance was improved to satisfy the design requirements.

Original languageEnglish
Pages (from-to)106-111
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume23
Issue number1
StatePublished - Jan 2008
Externally publishedYes

Keywords

  • Aerospace propulsion system
  • Artificial neural network
  • Genetic algorithm
  • Optimization design under multiple working conditions
  • Turbine

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