Large-scale CFD optimization based on the FFD parametrization using the multipoint approximation method in an HPC environment

Yury M. Korolev, Vassili V. Toropov, Shahrokh Shahpar

Research output: Chapter or section in a book/report/conference proceedingChapter in a published conference proceeding

11 Citations (SciVal)

Abstract

An adaptation of the Multipoint Approximation Method (MAM) to a high-performance computing (HPC) environment is presented and demonstrated by high-fidelity CFD-based design optimization of a highly-loaded transonic rotor, significantly improving its efficiency in a much reduced design time. MAM is incorporated into the Rolls-Royce SOPHY design system, used in this study, that includes the free-form deformation (FFD) parametrization of the blade shape, automatic meshing, CFD analysis, and post-processing.

Original languageEnglish
Title of host publication16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Place of PublicationU. S. A.
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624103681
DOIs
Publication statusPublished - 22 Jun 2015
Event16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 - Dallas, USA United States
Duration: 22 Jun 201526 Jun 2015

Publication series

Name16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

Conference

Conference16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015
Country/TerritoryUSA United States
CityDallas
Period22/06/1526/06/15

Bibliographical note

Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rigths reserved.

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

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