Finite element analysis of a thin walled composite wing by including warping effects

Ozdemir Ozgumus, Seher Durmaz, Metin Orhan Kaya

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The purpose of the present paper is to develop a finite element code to model a thin-walled composite beam. The beam is modeled as a thin-walled composite beam with a single-cell, rectangular cross-section featuring both CAS and CUS lay-up configurations. Analytical and finite element formulations of the flapwise bending, chordwise bending and torsional displacements of the beam are derived. Effect of the ply orientation on the natural frequencies is investigated and it is noticed that the obtained results are in good agreement with the ones in open literature.

Original languageEnglish
Title of host publicationSound, Vibration and Design
PublisherAmerican Society of Mechanical Engineers (ASME)
Pages209-214
Number of pages6
ISBN (Print)9780791844502
DOIs
Publication statusPublished - 2010
EventASME 2010 International Mechanical Engineering Congress and Exposition, IMECE 2010 - Vancouver, BC, Canada
Duration: 12 Nov 201018 Nov 2010

Publication series

NameASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
Volume13

Conference

ConferenceASME 2010 International Mechanical Engineering Congress and Exposition, IMECE 2010
Country/TerritoryCanada
CityVancouver, BC
Period12/11/1018/11/10

Fingerprint

Dive into the research topics of 'Finite element analysis of a thin walled composite wing by including warping effects'. Together they form a unique fingerprint.

Cite this