Search engine for discovering works of Art, research articles, and books related to Art and Culture
Javascript must be enabled to continue!
Multi-configuration Stiffened Panels under Compressive Load: Part 1 – Theoretical Analysis
View through CrossRef
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 cross-sectional area, their critical loads were not identical.
Science Publishing Corporation
Title: Multi-configuration Stiffened Panels under Compressive Load: Part 1 – Theoretical Analysis
Description:
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 cross-sectional area, their critical loads were not identical.
Related Results
A study of parametric instability of eccentrically stiffened rectangular plates
A study of parametric instability of eccentrically stiffened rectangular plates
The purpose of the investigation was to determine the onset of parametric instability for a simply-supported rectangular stiffened plate subjected to periodic in-plane loads. The s...
FABRICATION OF COMPOSITE STIFFENED PANEL
FABRICATION OF COMPOSITE STIFFENED PANEL
A Composite materials are widely used in aerospace structures due to their high strength-to weight ratio and high stiffness-to-weight ratio as compared to conventional materials.We...
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum LoadinThe paper describes methodology of numerical simulation of fatigue...
Comparative Study of Post-Buckling Load Redistribution in Stiffened Aircraft Panel With and Without Material Nonlinearity
Comparative Study of Post-Buckling Load Redistribution in Stiffened Aircraft Panel With and Without Material Nonlinearity
In this article, a comparative study is presented on the post-buckling load redistribution in stiffened aircraft panels modeled with and without material nonlinearity. In the first...
Dynamic Response of a Box Multistage Stiffened Beam under the Coupling of Vehicle Load and Air Blast Load
Dynamic Response of a Box Multistage Stiffened Beam under the Coupling of Vehicle Load and Air Blast Load
If a bridge is subjected to a blast load when there is vehicle traffic, not only its own safety is threatened, but it can also lead to damage to vehicles. In addition, the coupling...
Stability Analysis of Orthogonally Stiffened TLP Columns
Stability Analysis of Orthogonally Stiffened TLP Columns
Abstract
After completion of fabrication and prior to installation of the Auger tension leg platform (TLP), the designers became concerned that the hull's ring st...
Buckling Design of Ring-Stiffened Cylinders
Buckling Design of Ring-Stiffened Cylinders
ABSTRACT
The paper reports on a study carried out by J.P. Kenny & Partners on behalf of the U.K. Department of Energy to update the Guidance Notes relating to...
Crane Load Moment System For Offshore Crane Operations
Crane Load Moment System For Offshore Crane Operations
Abstract
History has shown that dependency upon the crane operator to monitor loads and boom angle or load radius do not allow the margin necessary to perform the...