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/10.1088/1742-6596/1005/1/012008Additional details
Identifiers
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