2012 ©
             Publication
Journal Publication
Title of Article Reliability-Based Design of an AircraftWing Using a Fuzzy-Based Metaheuristic 
Date of Acceptance 11 July 2021 
Journal
     Title of Journal Applied Sciences 
     Standard ISI 
     Institute of Journal Multidisciplinary Digital Publishing Institute (MDPI) 
     ISBN/ISSN 2076-3417 
     Volume
     Issue Volume 11, Issue 14 
     Month July
     Year of Publication 2021 
     Page 1-14 
     Abstract 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 overcome difficult tasks from the original probabilistic problem. The design problem is to minimize mass of a composite aircraft wing subject to aeroelastic and structural constraints through consideration of the material properties are the uncertainties. The design variables include aircraft wing structure dimensions. The reliability-based design approach is needed to alleviate such a problem. Due to the complexity of the aircraft wing structures design and aeroelastic analysis, nonprobability-based design is an alternative choice to increase computational efficiency in the design process. The optimum results show the efficiency of our proposed approach. 
     Keyword reliability-based design; aeroelasticity; optimization; aircraft wing; optimization technique; metaheuristics 
Author
627040019-1 Mr. SEKSAN WINYANGKUL [Main Author]
Engineering Doctoral Degree

Reviewing Status มีผู้ประเมินอิสระ 
Status ตีพิมพ์แล้ว 
Level of Publication นานาชาติ 
citation true 
Part of thesis true 
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