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23442

Surrogate-Based Aerodynamic Design Optimization: Use of Surrogates in Aerodynamic Design Optimization

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Last updated: 04 Jan 2025

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Abstract

The role of optimization in various practical applications has been increasing over the years. In the field of aerodynamics, design optimization is rapidly evolving in many ways. One of the latest developments in this field is the introduction of surrogates or metamodels. The use of surrogates has a number of advantages especially concerning the computation cost, memory and time budgets. The present paper aims to introduce the topic of surrogate-based optimization. An overview on the main aspects of surrogates and the associated terminology are discussed in detail. In addition, the paper provides a survey over the previous efforts contributing in this field. The paper is finalized with some general recommendations.

DOI

10.21608/asat.2009.23442

Keywords

Aerodynamic design optimization, Computational Fluid Dynamics, Surrogate modeling

Authors

First Name

M.

Last Name

Ahmed

MiddleName

Y. M.

Affiliation

PhD Student, Department of Mechanical Engineering, University of Sheffield.

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First Name

N.

Last Name

Qin

MiddleName

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Affiliation

Professor of Aerodynamics and Fluid Mechanics, Department of Mechanical Engineering, University of Sheffield, Senior Member AIAA.

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Volume

13

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May 26 – 28, 2009

Related Issue

4377

Issue Date

2009-05-01

Receive Date

2019-01-02

Publish Date

2009-05-01

Page Start

1

Page End

26

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_23442.html

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https://asat.journals.ekb.eg/service?article_code=23442

Order

4

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Surrogate-Based Aerodynamic Design Optimization: Use of Surrogates in Aerodynamic Design Optimization

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Article

Created At

22 Jan 2023