SS-V: 4010 Bimetallic Cantilever Beam

Test No. VTL02 Determine the displacements at the centerline at free end and bending stress at outer fiber for a bimetallic cantelever beam.


A cantilever beam is built from two equal thickness layers of different metals (Figure 1). The beam is fixed at centerline at one end (translations and rotation around the centerline are set to zero) and is subjected to uniform temperature change of 100 degrees Fahrenheit.

Both layers of materials have the same dimensions 10 x 1 x 0.05 inch.

The material properties are:
Modulus of Elasticity
3.e+7 psi
Poisson's Ratio
Coefficient of thermal expansion: top layer
2.e-5 in/in-F
Coefficient of thermal expansion: bottom layer
1.e-5 in/in-F

Figure 1.


Layers of the beam are simulated by solids glued together. In order to reproduce as close as possible boundary conditions of beam theory used in reference, the edge at centerline at “fixed” end of the beam is constrained in lateral directions. To eliminate rotations around the edge and sliding along the edge a point at the corner of upper fiber is fixed in two directions (Figure 2).

Because the beam is simulated using full 3D solid model, the constraints applied at the beam “fixed” end introduce local disturbances which quickly dissipate along the beam axis (Figure 4).

Figure 2. Constraints at ‘fixed” end

Figure 3. Beam deformation

Figure 4. Distribution of bending stress X at “fixed” end
  Ref Solution SimSolid % Difference
Free End, Middle Fiber, Disp X [in] 1.5000E-02 1.5020E-02 0.13%
Free End, Middle Fiber, Disp Y [in] 7.5000E-01 7.4950E-01 -0.07%
Top Fiber, Stress [psi] 7.5000E+03 7.4530E+03 -0.63%
1 R.J. Roark, W.C. Young, Formulas for Stress and Strain, 5th Edition, McGraw-Hill Book Co., Inc., New York, NY, 1975, pp. 113-114.