Bernoulli Cantilever Beam - GCMLab/GCMLab-FEM GitHub Wiki
Geometry and Mesh
Rectangular domain. 8 m long, 0.5 m tall. Q4 elements. A fine mesh density is applied to avoid shear locking. 200 elements along the length x 20 elements across the width.
Material properties
Parameter | Value |
---|---|
Young's Modulus | 200 GPa |
Poisson's ratio | 0.3 |
Thickness | 1 m |
Plane stress conditions applied
Applied loads
A traction of -400 kPa is applied to the y- degrees of freedom along the left edge (x=L), and traction free conditions are applied elsewhere.
Boundary conditions
All the x- and y- degrees of freedom along the left edge (x = 0) are fixed.
Solution
The displacement of the cantilever beam is given by the analytical Bernoulli solution.
where u_y is the vertical displacement, P is the total applied force on the end of the beam, L is the beam length, E is the elastic modulus, I is the moment of inertia, t is the beam thickness, and w is the beam width.
Given the prescribed inputs, the displacement at the end of the bar is -16.4 mm.