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 language | English |
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Title of host publication | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference |
Place of Publication | U. S. A. |
Publisher | American Institute of Aeronautics and Astronautics Inc. |
ISBN (Print) | 9781624103681 |
DOIs | |
Publication status | Published - 22 Jun 2015 |
Event | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 - Dallas, USA United States Duration: 22 Jun 2015 → 26 Jun 2015 |
Publication series
Name | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference |
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Conference
Conference | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 |
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Country/Territory | USA United States |
City | Dallas |
Period | 22/06/15 → 26/06/15 |
Bibliographical note
Publisher Copyright:© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rigths reserved.
ASJC Scopus subject areas
- Aerospace Engineering
- Mechanical Engineering