Lecture 3
Lecture 3.1: Low stiffness in polymers
Polymers: chain-like structures of repetitive units bonded along C-C backbone
Key features:
- The composition of the repetitive unit (the monomer)
- The number of linked units (the molecular weight)
- a linear backbone or a crosslinked backbone
Two types of polymers
Thermoplastics: the chains are connected through weak van der Waals forces
Thermosets: the chains are connected through weak van der Waals forces and strong covalent bonds
called crosslinks
Because of entropy most polymers like their molecules to coil up in a random structure. Now,
deformation of such a polymer does proceed via the rotation of segments of the molecule.
Amorphous (disordered) polymers: transparent
Semi-crystalline (ordered) polymers: translucent
Stretching polymers
Unstretched: more anisotropic
Stretched: chain orientation, more anisotropy and higher stiffness
The modulus of polymers
The modulus of polymers depends more on average molecular alignment than on composition.
In crosslinked polymers composition and crosslinking density have relative high impact.
The structure and therefore the elastic properties can be anisotropic
The consequences for the temperature dependence of E-modulus of polymers
Lecture 3.2: The mid-high stiffness in hybrids (composites)
Hybrid properties
Properties of composites are bound by the property values of the constituents
UD fibre reinforced matrices
Under an external axial load parallel to the fibres the strain in the fibres is the same as the strain in
the matrix
The forces required to strain the fibres F fibres = ff * A0 * Ef * , where ff is fibre fraction
The force required to strain the matrix Fmatrix = (1-ff) * Ao * Em *
The total force Fcompos = Ffibres + Fmatrix
Hence: Fcompos / A0 = ff * Ef * + (1-ff) * Em *
or
Under an external axial load perpendicular to the fibres the stress in the fibre is the same as the
stress in the matrix
By analogous analysis
Changing performance by going porous
Lecture 3.3: Stiffness-limited design
Separating the effects of shape (+ dimensions) and material on stiffness of the product
Three common loads of modes of loading
- Tie with a circular cross-section loaded in tension
- Beam with a rectangular cross-section loaded in bending
- Shaft of circular cross-section loaded in torsion
Stiffness of a tie rod loaded in tension
Relation between load F, deflection and stiffness S
Shape of cross-section does not matter because the stress is uniform across the section
Buckling of columns and plates under axial compression
If sufficiently slender, an elastic column or plate, loaded in compression fails by elastic buckling at a
critical load
Value of n depends on the end constraints of the beam
Elastic bending of beams
Curvature of initially straight axis
Stress caused by bending moment in a beam with a given Young’s modulus
Second moment of area
Shape matters: the material resists better bending the further is from the neutral axis
I characterizes the bending resistance of the section (includes the size and the shape)
Elastic stiffness of a beam under transverse loading
C1 is the only value that depends on the beam supports and the distribution of the load