High performance 3-node shell element for linear and geometrically nonlinear analysis of composite laminates
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: Composites Part B: Engineering (151:) - Amsterdam [u.a.] : Elsevier - S. 118-126
- Event
-
Veröffentlichung
- (where)
-
Berlin
- (who)
-
Technische Universität Berlin
- (when)
-
2020
- Creator
-
Rama, Gil
Marinković, Dragan
Zehn, Manfred
- DOI
-
10.14279/depositonce-10663
- Handle
-
11303/11775
- URN
-
urn:nbn:de:101:1-2020102800582768708148
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:26 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Rama, Gil
- Marinković, Dragan
- Zehn, Manfred
- Technische Universität Berlin
Time of origin
- 2020
Other Objects (12)
A geometrically nonlinear Hellinger–Reissner shell element for the postbuckling analysis of variable stiffness composite laminate structures
Geometrically correct laminated composite shell modeling : dynamic variational asymptotic procedures
Efficient three-node finite shell element for linear and geometrically nonlinear analyses of piezoelectric laminated structures
Geometrically non-linear theories of thin elastic shells
Geometrically exact shell theory from a hierarchical perspective
Geometrically nonlinear analysis and vibration of in-plane-loaded variable angle tow composite plates and shells
Mechanism Based Constitutive Model for Composite Laminates
Design and Ballistic Performance of Hybrid Composite Laminates
Computing laminate composite voxel properties using Mirtich formulas
Stacking sequences in composite laminates through design optimization
Flexural vibrations of geometrically nonlinear composite beams with interlayer slip
Modelling low velocity impact induced damage in composite laminates
A geometrically nonlinear Hellinger–Reissner shell element for the postbuckling analysis of variable stiffness composite laminate structures
Geometrically correct laminated composite shell modeling : dynamic variational asymptotic procedures
Efficient three-node finite shell element for linear and geometrically nonlinear analyses of piezoelectric laminated structures
Geometrically non-linear theories of thin elastic shells
Geometrically exact shell theory from a hierarchical perspective
Geometrically nonlinear analysis and vibration of in-plane-loaded variable angle tow composite plates and shells
Mechanism Based Constitutive Model for Composite Laminates
Design and Ballistic Performance of Hybrid Composite Laminates
Computing laminate composite voxel properties using Mirtich formulas
Stacking sequences in composite laminates through design optimization
Flexural vibrations of geometrically nonlinear composite beams with interlayer slip
Modelling low velocity impact induced damage in composite laminates
A geometrically nonlinear Hellinger–Reissner shell element for the postbuckling analysis of variable stiffness composite laminate structures
Geometrically correct laminated composite shell modeling : dynamic variational asymptotic procedures
Efficient three-node finite shell element for linear and geometrically nonlinear analyses of piezoelectric laminated structures
Geometrically non-linear theories of thin elastic shells
Geometrically exact shell theory from a hierarchical perspective
Geometrically nonlinear analysis and vibration of in-plane-loaded variable angle tow composite plates and shells
Mechanism Based Constitutive Model for Composite Laminates
Design and Ballistic Performance of Hybrid Composite Laminates
Computing laminate composite voxel properties using Mirtich formulas
Stacking sequences in composite laminates through design optimization
Flexural vibrations of geometrically nonlinear composite beams with interlayer slip