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Efficient multipoint aerodynamic design optimization via cokriging

Efficient multipoint aerodynamic design optimization via cokriging
Efficient multipoint aerodynamic design optimization via cokriging
Multipoint objective functions are often employed within aerodynamic optimizations to prevent a reduction in offdesign performance. However, this typically results in the need for a significant number of simulations at a variety of design conditions to calculate the objective function. The following paper attempts to address this problem through the application of a multilevel cokriging model within the optimization process. A large number of single-point design simulations are augmented by a smaller number of multipoint simulations. The technique is shown to result in surrogate models as effective as those produced using a traditional multipoint process when optimizing a transonic airfoil but with a reduction in the total number of simulations
0021-8669
1685-1695
Toal, David J.J.
dc67543d-69d2-4f27-a469-42195fa31a68
Keane, Andy J.
26d7fa33-5415-4910-89d8-fb3620413def
Toal, David J.J.
dc67543d-69d2-4f27-a469-42195fa31a68
Keane, Andy J.
26d7fa33-5415-4910-89d8-fb3620413def

Toal, David J.J. and Keane, Andy J. (2011) Efficient multipoint aerodynamic design optimization via cokriging. Journal of Aircraft, 48 (5), 1685-1695. (doi:10.2514/1.C031342).

Record type: Article

Abstract

Multipoint objective functions are often employed within aerodynamic optimizations to prevent a reduction in offdesign performance. However, this typically results in the need for a significant number of simulations at a variety of design conditions to calculate the objective function. The following paper attempts to address this problem through the application of a multilevel cokriging model within the optimization process. A large number of single-point design simulations are augmented by a smaller number of multipoint simulations. The technique is shown to result in surrogate models as effective as those produced using a traditional multipoint process when optimizing a transonic airfoil but with a reduction in the total number of simulations

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Published date: 1 September 2011
Organisations: Computational Engineering & Design Group

Identifiers

Local EPrints ID: 204251
URI: http://eprints.soton.ac.uk/id/eprint/204251
ISSN: 0021-8669
PURE UUID: 89b30efd-47cc-4ed7-8774-28a46f4b7162
ORCID for David J.J. Toal: ORCID iD orcid.org/0000-0002-2203-0302
ORCID for Andy J. Keane: ORCID iD orcid.org/0000-0001-7993-1569

Catalogue record

Date deposited: 25 Nov 2011 14:14
Last modified: 15 Mar 2024 03:29

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