Консоль из круглого стержня нагружена внецентренной нормальной силой. Determine the maximum vertical deflection of the console using the geometrically linear and second-order analysis.
На консоль из круглого стержня действует внецентренная поперечная сила. Determine the maximum deflection and maximum twist of the console using the geometrically linear analysis.
На консоль из круглого стержня действует внецентренная равномерная нагрузка. Determine the maximum deflection and maximum twist of the console using the geometrically linear analysis.
Данный контрольный пример основан на контрольном примере 0122. A single-mass system without damping is subjected to an axial loading force. An ideal elastic-plastic material with characteristics is assumed. Determine the time course of the end-point deflection, velocity, and acceleration.
Симметричная конструкция мелкого заложения состоит из восьми одинаковых ферм, встроенных в шарнирные опоры. The structure is loaded by a concentrated force and alternatively by imposed nodal deformation over the critical limit point when the snap-through occurs. Imposed nodal deformation is used in RFEM 5 and RSTAB 8 to obtain the full equilibrium path of the snap-through. The self-weight is neglected in this example. Determine the relationship between the actual loading force and the deflection, considering large deformation analysis. Evaluate the load factor at the given deflections.
Труба с трубчатым сечением загружена внутренним давлением. This internal pressure causes axial deformation of the pipe (the Bourdon effect). Determine the axial deformation of the pipe endpoint.
Конструкция состоит из четырех ферм, встроенных в шарнирные опоры. The structure is loaded by a concentrated force and alternatively by imposed nodal deformation over the critical limit point, when snap-through occurs. Imposed nodal deformation is used in RFEM 5 and RSTAB 8 to obtain the full equilibrium path of the snap-through. The self-weight is neglected in this example. Determine the relationship between the actual loading force and the deflection, considering large deformation analysis. Evaluate the load factor at given deflections.
Между двумя опорами подвешены очень жесткие канаты. Determine the equilibrium shape of the cable (the catenary), consider the gravitational acceleration, and neglect the stiffness of the cable. Verify the position of the cable at the given test points.
- 000120
- Расчет
- RFEM 5
-
- RSTAB 8
- RF-DYNAM Pro | Natural Vibrations 5
- RF-DYNAM Pro | Forced Vibrations 5
- RF-DYNAM Pro | Equivalent Loads 5
- RF-DYNAM Pro | Nonlinear Time History 5 (нелинейное изменение во времени)
- DYNAM Pro | Natural Vibrations 8 (собственные колебания)
- DYNAM Pro | Equivalent Loads (Эквивалентные нагрузки) 8
- DYNAM Pro | Nonlinear Time History 8
Система единичных масс с амортизатором находится под действием постоянной силы нагрузки. Determine the deflection and velocity of the dashpot endpoint in the given test time.
- 000112
- Расчет
- RFEM 5
-
- RSTAB 8
- RF-DYNAM Pro | Natural Vibrations 5
- RF-DYNAM Pro | Forced Vibrations 5
- RF-DYNAM Pro | Equivalent Loads 5
- RF-DYNAM Pro | Nonlinear Time History 5 (нелинейное изменение во времени)
- DYNAM Pro | Natural Vibrations 8 (собственные колебания)
- DYNAM Pro | Equivalent Loads (Эквивалентные нагрузки) 8
- DYNAM Pro | Nonlinear Time History 8
Тонкая строка натянута вследствие начальной деформации и сначала отклонена. Determine the deflection of the test point at the given test times.
Цель данного примера - продемонстрировать необратимые процессы, вызванные трением. After the loading and unloading, the end-point is in a different position than where it was at the beginning. Determine the movement of the node in the X direction.
Консоль загружена поперечной и осевой силой на правом конце и полностью защемлена на левом конце. The problem is described by the following set of parameters. The problem is solved by using the geometrically linear analysis, second-order analysis, and large deformation analysis.
Конструкция из двутаврового профиля полностью закреплена на левом конце и встроена в подвижную опору на правом конце. The structure consists of two segments. The self-weight is neglected in this example. Determine the maximum deflection of the structure, the bending moment on the fixed end, the rotation of segment 2, and the reaction force at point B by means of the geometrically linear analysis and the second-order analysis. The verification example is based on the example introduced by Gensichen and Lumpe.
К тому же, на свободном конце консоли действует момент, Using the geometrically linear analysis and large deformation analysis, and neglecting the beam's self-weight, determine the maximum deflections at the free end. The verification example is based on the example introduced by Gensichen and Lumpe.
Четыре колонны закреплены снизу и соединены жестким блоком наверху. The block is loaded by pressure and modeled by an elastic material with a high modulus of elasticity. The outer columns are modeled by linear elastic material and the inner columns by a stress-strain diagram with decaying dependence. Assuming only the small deformation theory and neglecting the structure's self-weight, determine its maximum deflection.
Конструкция из двутавровых ферм опирается на обоих концах пружинные скользящие опоры и нагружена поперечными силами. The self-weight is neglected in this example. Determine the deflection of the structure, the bending moment, the normal force in the given test points, and the horizontal deflection of the spring supports.
На левом конце поддерживается двутавровая консоль, которая нагружена крутящим моментом. 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).
Рассмотрим соединение труб строительных лесов, подверженное действию осевой силы и момента. Self-weight is not considered. The material of the tube is idealized as perfectly rigid. All geometrical non-linearities are ignored. Determine the angle of deflection.
A cantilever beam with an I-beam cross-section of length L is defined. The beam has five mass points with masses m acting in the X-direction. Собственный вес не учитывается. The frequencies, mode shapes, and equivalent loads of this 5-DOF system are analytically calculated and compared with the results from RSTAB and RFEM.
Стальная балка квадратного сечения с осевой нагрузкой имеет шарнирное закрепление на одном конце и подпружинивание - на другом. Two cases with different spring stiffnesses are considered. The verification example solves the calculation of the load factors of the beam in the image using the linear stability analysis.