Robust design of compressor fan blades against erosion
Robust design of compressor fan blades against erosion
This paper is concerned with robust aerodynamic design of compressor blades against erosion. The proposed approach combines a multiobjective genetic algorithm with geometry modeling methods, high-fidelity computational fluid dynamics, and surrogate models to arrive at robust designs on a limited computational budget. The multiobjective formulation used here allows explicit trade-off between the mean and variance of the performance to be carried out. Detailed numerical studies are presented for robust geometric design of a typical compressor fan blade section to illustrate the proposed methodology. The performance of a selected robust optimal solution on the Pareto front is compared to a deterministic optimal solution to demonstrate that significant improvements in the mean shift and variance can be achieved.
864-873
Kumar, Apurva
9152d989-0e22-4bba-a1f2-93aa080b8766
Keane, Andy J.
26d7fa33-5415-4910-89d8-fb3620413def
Nair, Prasanth B.
d4d61705-bc97-478e-9e11-bcef6683afe7
Shahpar, Shahrokh
eacd16f8-2e5f-4559-8d84-0c9c904d49a1
2006
Kumar, Apurva
9152d989-0e22-4bba-a1f2-93aa080b8766
Keane, Andy J.
26d7fa33-5415-4910-89d8-fb3620413def
Nair, Prasanth B.
d4d61705-bc97-478e-9e11-bcef6683afe7
Shahpar, Shahrokh
eacd16f8-2e5f-4559-8d84-0c9c904d49a1
Kumar, Apurva, Keane, Andy J., Nair, Prasanth B. and Shahpar, Shahrokh
(2006)
Robust design of compressor fan blades against erosion.
Journal of Mechanical Design, 128 (4), .
(doi:10.1115/1.2202886).
Abstract
This paper is concerned with robust aerodynamic design of compressor blades against erosion. The proposed approach combines a multiobjective genetic algorithm with geometry modeling methods, high-fidelity computational fluid dynamics, and surrogate models to arrive at robust designs on a limited computational budget. The multiobjective formulation used here allows explicit trade-off between the mean and variance of the performance to be carried out. Detailed numerical studies are presented for robust geometric design of a typical compressor fan blade section to illustrate the proposed methodology. The performance of a selected robust optimal solution on the Pareto front is compared to a deterministic optimal solution to demonstrate that significant improvements in the mean shift and variance can be achieved.
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kuma_06.pdf
- Accepted Manuscript
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Published date: 2006
Identifiers
Local EPrints ID: 41987
URI: http://eprints.soton.ac.uk/id/eprint/41987
ISSN: 1050-0472
PURE UUID: 290ffba8-916c-499a-9307-199608a55196
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Date deposited: 25 Oct 2006
Last modified: 16 Mar 2024 02:53
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Contributors
Author:
Apurva Kumar
Author:
Prasanth B. Nair
Author:
Shahrokh Shahpar
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