Zobrazeno 1 - 10
of 43
pro vyhledávání: '"Suwin Sleesongsom"'
Autor:
Pakin Phromphan, Jirachot Suvisuthikasame, Metas Kaewmongkol, Woravech Chanpichitwanich, Suwin Sleesongsom
Publikováno v:
Symmetry, Vol 16, Iss 7, p 901 (2024)
This research paper presents a new Latin hypercube sampling method, aimed at enhancing its performance in quantifying uncertainty and reducing computation time. The new Latin hypercube sampling (LHS) method serves as a tool in reliability-based desig
Externí odkaz:
https://doaj.org/article/0eec5846362748139bcb3a8a45f65452
Autor:
Noppawit Kumkam, Suwin Sleesongsom
Publikováno v:
Aerospace, Vol 11, Iss 6, p 435 (2024)
This research proposes an efficient technique for reliability-based topology optimization (RBTO), which deals with uncertainty and employs proportional topology optimization (PTO) to achieve the optimal reliability structure. The recent technique, ca
Externí odkaz:
https://doaj.org/article/fdb98c3c81644dab8586f79bc6ceaf47
Publikováno v:
Symmetry, Vol 15, Iss 2, p 305 (2023)
Reliability-based partial topology optimization (RBPTO) is a new approach for aircraft structural design; however, it brings computational complexity and makes aeroelasticity analysis quite challenging. Therefore, the present study proposed the multi
Externí odkaz:
https://doaj.org/article/ccc8179c3b05405686d93745b84d8445
Publikováno v:
Symmetry, Vol 14, Iss 10, p 2125 (2022)
The multi-objective reliability-based design optimization (MORBDO) of an aircraft structure employing a non-probabilistic model, at present, still has a high level of analysis complexity while solving the possibility safety index (PSI) as they are a
Externí odkaz:
https://doaj.org/article/e117791fd1dc423daae51c1794f2b97b
Autor:
Seksan Winyangkul, Kittinan Wansaseub, Suwin Sleesongsom, Natee Panagant, Sumit Kumar, Sujin Bureerat, Nantiwat Pholdee
Publikováno v:
Metals, Vol 11, Iss 8, p 1311 (2021)
This paper presents multi-objective topology and sizing optimization of a morphing wing structure. The purpose of this paper is to design a new aircraft wing structure with a tapered shape for ribs, spars, and skins including a torsion beam for exter
Externí odkaz:
https://doaj.org/article/832e1c41e79d4f8a9a5f2c0d03c42de7
Publikováno v:
Applied Sciences, Vol 11, Iss 14, p 6463 (2021)
The purpose of this paper is to design aircraft wing using reliability-based design optimization concerned to fuzzy uncertainty variables. A possibilistic safety index-based design optimization (PSIBDO) with fuzzy uncertainties is proposed to overcom
Externí odkaz:
https://doaj.org/article/e367e78baf334ccbb6e4e65d76cc2f22
Autor:
Poothanet Chabphet, Supanat Santichatsak, Tunnatorn Na Thalang, Suwin Sleesongsom, Sujin Bureerat
Publikováno v:
Proceedings, Vol 39, Iss 1, p 5 (2019)
This paper proposes an approach to synthesize a high-lift mechanism (HLM) of a transportation aircraft. Such a mechanism is very important for generation of additional lift to an aircraft wing during take-off and landing. The design problem is minimi
Externí odkaz:
https://doaj.org/article/fa943d949b60452fa86d454d49329030
Autor:
Prasert Prapamonthon, Soemsak Yooyen, Suwin Sleesongsom, Daniele Dipasquale, Huazhao Xu, Jianhua Wang, Zhaoqing Ke
Publikováno v:
Energies, Vol 11, Iss 4, p 1000 (2018)
The aim of this paper is to numerically investigate cooling performances of a non-film-cooled turbine vane coated with a thermal barrier coating (TBC) at two turbulence intensities (Tu = 8.3% and 16.6%). Computational fluid dynamics (CFD) with conjug
Externí odkaz:
https://doaj.org/article/daabf6f2383244b6a635f44ae6f93c44
Autor:
Suwin Sleesongsom, Sujin Bureerat
Publikováno v:
Applied Sciences, Vol 8, Iss 2, p 271 (2018)
This paper aims to study the comparative performance of original multi-objective population-based incremental learning (MPBIL) and three improvements of MPBIL. The first improvement of original MPBIL is an opposite-based concept, whereas the second a
Externí odkaz:
https://doaj.org/article/890e33ab5464401fba8a3427dc615b50
Autor:
Suwin Sleesongsom, Sujin Bureerat
Publikováno v:
Journal of Engineering, Vol 2013 (2013)
The objective of this research is to propose a new reduced-order modeling method. This approach is based on fluid eigenmodes and body vortices without using static correction. The vortex lattice method (VLM) is used to analyze unsteady flows over two
Externí odkaz:
https://doaj.org/article/b50d5c3c2fac4f4d8ba1da95137a404c