Tutorial 10 - ETH - Laboratory of Composite Materials and Adaptive

Mechanics of Composite Materials
Tutorial 10
Autumn Semester 2014
Hand-out:
08.12.2014
Tutorial 10: Beam
with Shear-Compliant Core
Introduction
As schematically shown in Figure 1, it may be distinguished between transverse and in-plane deformations induced by shear. These are assumed to
act exclusively in the core (GD = ∞) as well as being linear (EK << ED ),
which results in constant shear strains and stresses in the core.
Figure 1: Shear deformations of a sandwich element.
Figure 2: Cross-section of a sandwich beam.
ETH Zurich
Laboratory of Composite Materials
and Adaptive Structures
I. Kuder
1
Mechanics of Composite Materials
Tutorial 10
Autumn Semester 2014
dws
· d = (γ − γ0 ) · tk
dx
dws
tk
γtk γ0 tk
= (γ − γ0 ) =
−
=
dx
d
d
d
Z
ws =
x
(
0
τk
Gk t k
d
−
γ0 tk
τk dtk γ0 tk
Q γ0 tk
=
−
= −
d
Gk d2
d
S
d
Q γ0 tk
MB
γ0 t k
−
) dx =
−
x + const
S
d
S
d
The two unknowns arise from the boundary conditions.
The aim of the following two exercises is to show that a shear loading may
induce unexpected displacements of a shear-compliant core.
Exercise 1
Consider a sandwich beam symmetrically loaded by a force P, as shown in
Figure 3, and characterised by cross-sectional dimensions found in Figure 2.
Assuming that the constituent pure bending deflection is much smaller than
the pure shear displacement (wb ws ) and hence negligible (w ≈ ws ), determine the deflection of the beam using the above general formula describing
the displacement arising from the shear deformation of the core.
Figure 3: Symmetrically loaded sandwich beam with a shear-compliant core.
ETH Zurich
Laboratory of Composite Materials
and Adaptive Structures
I. Kuder
2
Mechanics of Composite Materials
Autumn Semester 2014
Tutorial 10
Exercise 2:
Consider an unsymmetrically loaded beam presented in Figure 4, with the
same cross-sectional configuration as before (Figure 2). Determine the shearinduced constituent deflection, assuming negligibility of bending displacement. Provide a qualitative plot of the deformed structure.
Figure 4: Unsymmetrically loaded sandwich beam with a shear-compliant
core.
ETH Zurich
Laboratory of Composite Materials
and Adaptive Structures
I. Kuder
3