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...

Celý popis

Uložené v:

Podrobná bibliografia
Vydané v:	International journal of aeronautical and space sciences Ročník 21; číslo 3; s. 723 - 732
Hlavní autori:	Wansaseub, K., Sleesongsom, S., Panagant, N., Pholdee, N., Bureerat, S.
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Seoul The Korean Society for Aeronautical & Space Sciences (KSAS) 01.09.2020 한국항공우주학회
Predmet:	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
On-line prístup:	Získať plný text
Tagy:	Pridať tag Žiadne tagy, Buďte prvý, kto otaguje tento záznam!

Buďte prvý, kto okomentuje tento záznam!