Publication detail

COMPARISON OF THREE TYPES OF IMPERFECTIONS APPLIED DURING BUCKLING ANALYSIS OF CYLINDRICAL SHELL UNDER COMPRESSIVE LOAD

MALIŠ, M. URÍK, T.

Original Title

COMPARISON OF THREE TYPES OF IMPERFECTIONS APPLIED DURING BUCKLING ANALYSIS OF CYLINDRICAL SHELL UNDER COMPRESSIVE LOAD

Type

conference paper

Language

English

Original Abstract

Thin-walled structures like unstiffened cylindrical shells are prone to buckling. The imperfections, deviation from ideal shape, loading path or cutouts can considerably reduce buckling load of the structure. Three types of imperfections have been considered and compared – geometrical imperfection represented by single perturbation load approach and two types of cutouts, the circular and the rectangular one. Abaqus standard software package have been used for analysis of cylindrical shells made from composite material.

Keywords

buckling, composite, CFRP, FAE, FEM, Abaqus

Authors

MALIŠ, M.; URÍK, T.

RIV year

2013

Released

22. 6. 2013

Publisher

Akademické nakladetelství CERM

Location

Brno

ISBN

978-80-7204-843-4

Book

New Trends in Civil Aviation 2013

Edition

2013

Pages from

63

Pages to

67

Pages count

5

BibTex

@inproceedings{BUT100708,
  author="Michal {Mališ} and Tomáš {Urík}",
  title="COMPARISON OF THREE TYPES OF IMPERFECTIONS APPLIED DURING BUCKLING ANALYSIS OF CYLINDRICAL SHELL UNDER COMPRESSIVE LOAD",
  booktitle="New Trends in Civil Aviation 2013",
  year="2013",
  series="2013",
  pages="63--67",
  publisher="Akademické nakladetelství CERM",
  address="Brno",
  isbn="978-80-7204-843-4"
}