Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor

Research output: Contribution to journalResearch articleContributedpeer-review

Contributors

  • Max Dittmann - , TUD Dresden University of Technology (Author)
  • Robin Schmidt - , Rolls-Royce Deutschland (Author)
  • Marcus Meyer - , Rolls-Royce Deutschland (Author)

Abstract

This paper applies the computationally advantageous combination of a differential analysis technique and the adjoint method in the context of uncertainty quantification to the gradient-based robust design optimization of aerofoils. First, the accuracy and feasibility of the method is evaluated using an analytical test function. The method is subsequently applied to the robust design optimization of a rotor blade under geometric uncertainty, that is based on a parametrized population of optically 3D scanned blades. A significant improvement of the robustness w.r.t. the isentropic efficiency of the rotor is reported.

Details

Original languageEnglish
Article number021010
Number of pages8
JournalJournal of Turbomachinery
Volume145
Issue number2
Early online date12 Oct 2022
Publication statusPublished - 1 Feb 2023
Peer-reviewedYes

External IDs

Scopus 85144303715

Keywords

Keywords

  • And turbine aerodynamic design, Compressor, Design under uncertainty, Robust design optimization, Turbomachinery blading design, computational fluid dynamics (CFD)