Buckling Analysis of Stiffened Composite Panels for Different Ply Orientations

Abstract

Buckling and post-buckling analysis was performed on composite stiffened panel using Abaqus/CAE to obtain the critical load and modes of failures, with different parameters like ply orientation, different composite materials, stiffeners & by changing the number of stiffeners were derived. To investigate the buckling behavior of composite curved stiffened panels, the nonlinear FE tools Abaqus/Explicit are employed. Studies were conducted using the analytical tool in order to understand the structural behavior in the post buckling range and to determine the critical parameters

Authors and Affiliations

N. MADHAVI, K. SREELAKSHMI, SUDHAKAR ATCHYUTUNI

Keywords

Related Articles

Design Optimization of Rotor Propulsive Delta Wing

The Wing Rotor Configuration is designed for the purpose of VTOL (vertical takeoff and landing) which is a combination of Delta wing and rotor together integrated at the empennage section of the aircraft wing. The model...

An Effect of Wall Corner Radius of Punch on the Features of the Hexagonal Cup Fabricated by the Deep Drawing Process

This work aims to study the effect of different deep drawing process parameters on the distribution of strain and thickness in deep drawing operation, such as wall corner radius of punch, the thickness of the sheet, and...

An Effect of SiO2 and Carbon Nano Tubes on Mechanical Properties of LM-12 Aluminium Alloy Hybrid Metal Matrix Composite

The present research is aimed to develop hybrid metal matrix composite using aluminium alloy LM-12 reinforced with constant weight percentage (9%) of SiO2 and different weight percentage (wt %) carbon nano tubes. After c...

Cycle Time Optimized Path Planning for Industrial Robot using Robomaster

The main aim of the paper is to demonstrate the optimal cycle time taken by a 6 axis industrial robot, by following the shortest path. Planning for path is important because, it allows knowing about the path traversal of...

Vibration Analysis of Composite Laminated Plates Using Higher Order Theory and Levy’s Solution

This paper represents the exploration on the response of a symmetric composite laminated plate. The properties like weight reduction, Fatigue life, wear resistance, Corrosion resistance, Strength Stiffness and Thermal pr...

Download PDF file
  • EP ID EP280242
  • DOI 10.24247/ijmperdfeb201881
  • Views 100
  • Downloads 0

How To Cite

N. MADHAVI, K. SREELAKSHMI, SUDHAKAR ATCHYUTUNI (2018). Buckling Analysis of Stiffened Composite Panels for Different Ply Orientations. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD ), 8(1), 745-752. https://europub.co.uk/articles/-A-280242