VM41

VM41
Small Deflection of a Rigid Beam

Overview

Reference:Any Basic Statics and Strength of Material Book
Analysis Type(s):Static Analysis (ANTYPE = 0)
Element Type(s):
Stiffness, Damping, or Mass Matrix Element (MATRIX27)
Bushing Element (COMBI250)
3D 2 Node Beam (BEAM188)
Input Listing:vm41.dat

Test Case

A very stiff beam of length L, subjected to a lateral load F, is initially at position AB on a horizontal table. Point A is pinned to the table and restrained from rotation by a relatively weak torsion spring. Determine the final position of the beam in terms of δx, δy, and Θ. Show that the bending stress in the beam σbend is negligible.

Figure 56: Rigid Beam Problem Sketch

Rigid Beam Problem Sketch

Material PropertiesGeometric PropertiesLoading
Kθz = 10,000 in-lb/rad
E = 30 x 106 psi
L = 10 in
F= 10 lb

Analysis Assumptions and Modeling Notes

The problem is solved using two approaches:

  • Thick beam geometry

  • Constraint equation

In the thick beam approach, the "rigid" beam properties are arbitrarily selected as area = 100 in2, I = 1000 in4, thickness = 10 in.

In the constraint equation approach, a constraint equation is used to enforce the assumption of a rigid beam. The constraint equation is of the form: δy = (L)(Θ). The beam properties are arbitrarily based on a 0.25 square inch cross-section.

The weak spring is modeled with either MATRIX27 or COMBI250.

Results Comparison

MATRIX27TargetMechanical APDLRatio
Thick BeamDeflectionx , in0.00.0-
Deflectiony , in-0.1-0.11.000
Angle, rad-0.01-0.011.000
Stressbend, psi0.00.03 [1]-
Constraint EquationDeflectionx , in0.00.0-
Deflectiony , in-0.1-0.11.000
Angle, rad-0.01-0.011.000
Stressbend , psi0.00.0-
COMBI250TargetMechanical APDLRatio
Thick BeamDeflectionx , in0.00.0-
Deflectiony , in-0.1-0.11.000
Angle, rad-0.01-0.011.000
Stressbend, psi0.00.03 [1]-
Constraint EquationDeflectionx , in0.00.0-
Deflectiony , in-0.1-0.11.000
Angle, rad-0.01-0.011.000
Stressbend , psi0.00.0-
  1. Small but negligible stress.