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A cantilever is loaded by a transversal and an axial force on the right end and is fully fixed on the left end. Das Problem wird durch folgenden Parametersatz beschrieben. The problem is solved by using the geometrically linear analysis, second-order analysis, and large deformation analysis.
A cantilever is loaded by a moment at its free end. Using the geometrically linear analysis and large deformation analysis, and neglecting the beam's self-weight, determine the maximum deflections at the free end. Dieses Verifikationsbeispiel basiert auf dem von Gensichen und Lumpe vorgestellten Beispiel.
Bestimmen Sie das Biegemoment, welches den Stab am freien Ende des Kragarms in eine kreisförmige Form biegt. Neglecting the beam's self-weight, assuming the large deformation analysis, and loading the cantilever with the moment, determine its maximum deflections.
Ein I-Profil-Kragträger ist am linken Ende gelagert und durch Moment belastet. The aim of this example is to compare the fixed support with the fork support and to investigate the behavior of some representative quantities. Comparison is also made to the solution by means of plates. Small deformations are considered, and the self-weight is neglected. Determine the rotation in the midpoint of the cantilever, and in case of the member entity with warping, determine the values of the primary torsional moment, the secondary torsional moment, and the warping moment both on the left end (point A) and the right end (point B).
A steel cantilever with a rectangular cross‑section is fully fixed on one side and free on the other. Das Ziel von diesem Verifizierungsbeispiel ist, die Eigenfrequenzen der Struktur zu ermitteln.
Weisen Sie nach, dass die Ergebnisse durch die Kopplung unterschiedlicher dimensionaler Elemente nicht beeinflusst werden. A cantilever with a rectangular cross-section is fixed at one end and loaded at the other by concentrated forces. Neglecting its self-weight and assuming only small deformations, determine the cantilever's maximum deflections.