Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 175-188 |
| Seitenumfang | 14 |
| Fachzeitschrift | Computational mechanics |
| Jahrgang | 13 |
| Ausgabenummer | 3 |
| Publikationsstatus | Veröffentlicht - Dez. 1993 |
| Extern publiziert | Ja |
Abstract
A numerical model for layered composite structures based on a geometrical nonlinear shell theory is presented. The kinematic is based on a multi-director theory, thus the in-plane displacements of each layer are described by independent director vectors. Using the isoparametric apporach a finite element formulation for quadrilaterals is developed. Continuity of the interlaminar shear stresses is obtained within the nonlinear solution process. Several examples are presented to illustrate the performance of the developed numerical model.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Numerische Mechanik
- Ingenieurwesen (insg.)
- Meerestechnik
- Ingenieurwesen (insg.)
- Maschinenbau
- Informatik (insg.)
- Theoretische Informatik und Mathematik
- Mathematik (insg.)
- Computational Mathematics
- Mathematik (insg.)
- Angewandte Mathematik
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in: Computational mechanics, Jahrgang 13, Nr. 3, 12.1993, S. 175-188.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - A nonlinear composite shell element with continuous interlaminar shear stresses
AU - Gruttmann, F.
AU - Wagner, W.
AU - Meyer, L.
AU - Wriggers, Peter
PY - 1993/12
Y1 - 1993/12
N2 - A numerical model for layered composite structures based on a geometrical nonlinear shell theory is presented. The kinematic is based on a multi-director theory, thus the in-plane displacements of each layer are described by independent director vectors. Using the isoparametric apporach a finite element formulation for quadrilaterals is developed. Continuity of the interlaminar shear stresses is obtained within the nonlinear solution process. Several examples are presented to illustrate the performance of the developed numerical model.
AB - A numerical model for layered composite structures based on a geometrical nonlinear shell theory is presented. The kinematic is based on a multi-director theory, thus the in-plane displacements of each layer are described by independent director vectors. Using the isoparametric apporach a finite element formulation for quadrilaterals is developed. Continuity of the interlaminar shear stresses is obtained within the nonlinear solution process. Several examples are presented to illustrate the performance of the developed numerical model.
UR - http://www.scopus.com/inward/record.url?scp=0027848409&partnerID=8YFLogxK
U2 - 10.1007/BF00370134
DO - 10.1007/BF00370134
M3 - Article
AN - SCOPUS:0027848409
VL - 13
SP - 175
EP - 188
JO - Computational mechanics
JF - Computational mechanics
SN - 0178-7675
IS - 3
ER -