Surrogate-Assisted Reliability Optimisation of an Aircraft Wing with Static and Dynamic Aeroelastic Constraints

This paper presents a numerical strategy for reliability-based design optimisation of an aircraft wing structure using a surrogate-assisted approach. The design problem is set to minimise aircraft wing mass subject to structural and aeroelastic constraints, while design variables are structural dime...

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Veröffentlicht in:	International journal of aeronautical and space sciences Jg. 21; H. 3; S. 723 - 732
Hauptverfasser:	Wansaseub, K., Sleesongsom, S., Panagant, N., Pholdee, N., Bureerat, S.
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Seoul The Korean Society for Aeronautical & Space Sciences (KSAS) 01.09.2020 한국항공우주학회
Schlagworte:	Aerospace Technology and Astronautics Engineering Fluid- and Aerodynamics Original Paper 항공우주공학 Multiobjective evolutionary algorithms Aeroelasticity Aircraft wing Reliability-based design optimisation
ISSN:	2093-274X, 2093-2480
Online-Zugang:	Volltext
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