Database
0012-B-Cantilever with end moment
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and published on 20.04.2018 on
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B0Classification
- ClassB · Numerical verification example
- Structural system typeBar structure - beam
- MechanicsStatics - third-order theory
- Material lawLinear elastic
- MaterialGeneral
- Verification formatDeformation verification
B1Problem description
A bending moment is applied to the end of the cantilever. When the load is increased to ML/2πEI=1.0, significant displacements and rotations occur in a geometrically non-linear analysis. Deformations are only possible in the XY plane. Deformations at the free end of the cantilever must be determined.
Material: linearly elastic; modulus of elasticity = 210,000 MPa; Poisson’s ratio = 0.0
Conditions: All degrees of freedom fixed at the supports
Load: ML/2πEI = 1.0
Der Kragarm wird am Kragarmende mit einem Biegemoment belastet. Durch Steigerung der Last bis auf ML/2πEI=1.0 treten bei geometrisch nichtlinearer Berechnung große Verschiebungen und Verdrehungen auf. Verformungen sind lediglich in der XY-Ebene möglich. Verformungen am freien Kragarmende sind zu ermitteln.
Material: linear-elastisch; E-Modul = 210000 MPa; Querdehnzahl = 0.0
Lagerung: Alle Freiheitsgrade an der Einspannung gehalten
Belastung: ML/2πEI = 1.0
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Register hereB5References
- [1] NAFEMS: Test NL5 from NAFEMS Publication NNB, Rev. 1, “NAFEMS Non-Linear Benchmarks”. Oktober. 1989.
- [2] Gruttmann, F.; Sauer, R.; Wagner, W.: A geometrical nonlinear eccentric 3D-beam element with arbitrary cross-sections. In: Computer Methods in Applied Mechanics and Engineering 160, 1998.
Editors
Krätzig & Partner Ingenieurgesellschaft für Bautechnik mbH (Bochum, Germany)
RIB Software GmbH (Stuttgart, Germany)
Dlubal Software GmbH (Tiefenbach, Germany)