Published April 1, 2018 | Version v1
Journal article

Buckling Analysis of Single and Multi Delamination In Composite Beam Using Finite Element Method

  • 1. Lightweight Structure Research Group, Faculty of Mechanical and Aerospace Engineering Institut Teknologi Bandung, Jl. Ganesha 10 Bandung 40132 (Indonesia)

Description

Delamination is one type of imperfection in structure which found usually in the composite structure. Delamination may exist due to some factors namely in-service condition where the foreign objects hit the composite structure and creates inner defect and poor manufacturing that causes the initial imperfections. Composite structure is susceptible to the compressive loading. Compressive loading leads the instability phenomenon in the composite structure called buckling. The existence of delamination inside of the structure will cause reduction in buckling strength. This paper will explain the effect of delamination location to the buckling strength. The analysis will use the one-dimensional modelling approach using two- dimensional finite element method. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1742-6596/1005/1/012008

Additional details

Publishing Information

Journal Title
Journal of Physics. Conference Series (Online)
Journal Volume
1005
Journal Issue
1
Journal Page Range
[10 p.]
ISSN
1742-6596

Conference

Title
5. International Seminar on Aerospace Science and Technology
Dates
27-29 Sep 2017
Place
Medan (Indonesia)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52090312
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
BUCKLING; DEFECTS; FINITE ELEMENT METHOD; MECHANICAL STRUCTURES; ONE-DIMENSIONAL CALCULATIONS; TWO-DIMENSIONAL CALCULATIONS
Descriptors DEC
CALCULATION METHODS; MATHEMATICAL SOLUTIONS; NUMERICAL SOLUTION