Multi-configuration stiffened panels under compressive load: Part 1 - Theoretical analysis

Stiffened panels are the structure used in the aircraft wing skin panels. Stiffened panels are often critical in compression load due to its thin structural configuration. This paper analyzes the critical loads of a multi configuration stiffened panels under axial compressive loading. The study comp...

Full description

Bibliographic Details
Main Authors: Ghani, A.R.A (Author), Kuntjoro, W. (Author), Muhammad, Z. (Author), Nasir, R.E.M (Author), Ramly, R. (Author)
Format: Article
Language:English
Published: Science Publishing Corporation Inc 2018
Subjects:
Online Access:View Fulltext in Publisher
View in Scopus
LEADER 01946nam a2200253Ia 4500
001 10.14419-ijet.v7i3.11.15926
008 220120s2018 CNT 000 0 und d
020 |a 2227524X (ISSN) 
245 1 0 |a Multi-configuration stiffened panels under compressive load: Part 1 - Theoretical analysis 
260 0 |b Science Publishing Corporation Inc  |c 2018 
490 1 |t International Journal of Engineering and Technology(UAE) 
650 0 4 |a Critical loads 
650 0 4 |a Moment of inertia 
650 0 4 |a Multiconfiguration stiffened panels 
650 0 4 |a Theoretical analysis 
856 |z View Fulltext in Publisher  |u https://doi.org/10.14419/ijet.v7i3.11.15926 
856 |z View in Scopus  |u https://www.scopus.com/inward/record.uri?eid=2-s2.0-85067271041&doi=10.14419%2fijet.v7i3.11.15926&partnerID=40&md5=ff1d237bb1a53b6f444853931e68ccc2 
520 3 |a Stiffened panels are the structure used in the aircraft wing skin panels. Stiffened panels are often critical in compression load due to its thin structural configuration. This paper analyzes the critical loads of a multi configuration stiffened panels under axial compressive loading. The study comprised three main sections; theoretical analysis, numerical analysis and experimental analysis. The present paper deals only with the theoretical analysis. This first part of analysis is very important since the results will be the main input parameter for the subsequent numerical and experimental analysis. The analysis was done on the buckling properties of the panels. Four panel configurations were investigated. Results showed that even though the stiffened panels have the same crosssectional area, their critical loads were not identical. © 2018 Authors. 
700 1 0 |a Ghani, A.R.A.  |e author 
700 1 0 |a Kuntjoro, W.  |e author 
700 1 0 |a Muhammad, Z.  |e author 
700 1 0 |a Nasir, R.E.M.  |e author 
700 1 0 |a Ramly, R.  |e author 
773 |t International Journal of Engineering and Technology(UAE)