Reliability-based design optimisation of an aircraft wing structure with high-fidelity modelling

Mel ike Nikbay; Muhammet Nasif Kuru; Semra Bayat; Necati Fakkusoglu

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Reliability-based design optimisation of an aircraft wing structure with high-fidelity modelling

机译：高保真建模的机翼结构基于可靠性的设计优化

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摘要

We present reliability-based design optimisation of a simple aircraft wing based on performance measure approach. Catia is used as a parametric solid modeller while Abaqus is used to compute the structural response of the wing system. As an optimisation driver, Modefrontier, is used with sequential quadratic programming method. The core of the problem leans on the structural optimisation of a statically loaded wing. Weight and first modal frequency of that wing are optimised with stochastic parameters. The uncertainties concerning both yield strength and Young's modulus of the aluminium material will be analysed by the reliability analysis code developed in Matlab.

机译：我们提出了一种基于性能评估方法的基于可靠性的简单飞机机翼的设计优化。 Catia被用作参数实体建模器，而Abaqus被用于计算机翼系统的结构响应。作为优化驱动程序，Modefrontier与连续二次编程方法一起使用。问题的核心在于静态载荷机翼的结构优化。该机翼的重量和第一模态频率通过随机参数进行优化。关于铝材的屈服强度和杨氏模量的不确定性将通过Matlab中开发的可靠性分析代码进行分析。

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来源
《International journal of design engineering》 |2010年第3期|p.247-259|共13页
作者
Mel ike Nikbay; Muhammet Nasif Kuru; Semra Bayat; Necati Fakkusoglu;
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作者单位

Department of Space Engineering,Faculty of Aeronautics and Astronautics,Istanbul Technical University,Ayazaga Campus, Maslak, 34469, Istanbul, Turkey;

Informatics Institute,Computational Science and Engineering,Istanbul Technical University,Ayazaga Campus, Maslak, 34469, Istanbul, Turkey;

Informatics Institute,Computational Science and Engineering,Istanbul Technical University,Ayazaga Campus, Maslak, 34469, Istanbul, Turkey;

Faculty of Aeronautics and Astronautics,Istanbul Technical University,Ayazaga Campus, Maslak, 34469, Istanbul, Turkey;

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原文格式 PDF
正文语种 eng
中图分类
关键词
structural optimisation; reliability analysis; aircraft wing; reliability-based design optimisation; RBDO; design engineering;

机译：结构优化;可靠性分析;飞机机翼;基于可靠性的设计优化;RBDO;设计工程;

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2. Improved Reliability-Based Optimization with Support Vector Machines and Its Application in Aircraft Wing Design [J] . Wang Yu, Yu Xiongqing, Du Xiaoping Mathematical Problems in Engineering . 2015,第PTa17期

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3. Improved Reliability-Based Optimization with Support Vector Machines and Its Application in Aircraft Wing Design [J] . YuWang, XiongqingYu, XiaopingDu Mathematical Problems in Engineering: Theory, Methods and Applications . 2015,第2期

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4. Model-based framework for multidisciplinary optimisation of early-stage aircraft wing design [C] . G. Pagliuca, T. Kipouros, A. M. Savill 2018 Applied Aerodynamics Conference . 2018

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5. A Robust and Reliability-Based Optimization Framework for Conceptual Aircraft Wing Design [D] . Paiva, Ricardo Miguel 2010

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6. A Method for Detecting Atmospheric Lagrangian Coherent Structures Using a Single Fixed-Wing Unmanned Aircraft System [O] . Peter J. Nolan, Hunter G. McClelland, Craig A. Woolsey, 2019

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8. L'Analyse Integrale de la Conception et l'Optimisation des Structures desAeronefs (Integrated Design Analysis and Optimisation of Aircraft Structures) [R] . 1992

机译：L'analyze Integrale de la Conception et l'Optimization des structures desaeronefs（飞机结构的综合设计分析和优化）

Reliability-based design optimisation of an aircraft wing structure with high-fidelity modelling

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