Detail publikace

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

MALIŠ, M. URÍK, T.

Originální název

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

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

buckling, composite, CFRP, FAE, FEM, Abaqus

Autoři

MALIŠ, M.; URÍK, T.

Rok RIV

2013

Vydáno

22. 6. 2013

Nakladatel

Akademické nakladetelství CERM

Místo

Brno

ISBN

978-80-7204-843-4

Kniha

New Trends in Civil Aviation 2013

Edice

2013

Strany od

63

Strany do

67

Strany počet

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"
}