Download - Micromechanics of Composite Materials
MDPN452Dr. Mohammad Tawfik
Mechanics of Composite Materials
MDPN452
Dr. Mohammad Tawfik
E-mail: [email protected]
MDPN452Dr. Mohammad Tawfik
Micromechanics
• The basic question of micromechanics is: what is the relationship of the composite material properties to the properties of the constituents?
MDPN452Dr. Mohammad Tawfik
The Design Question!
• How can the percentages of the constituent materials be varied so as to arrive at the desired composite stiffness and strength?
MDPN452Dr. Mohammad Tawfik
Definitions
• Macromechanics: The study of composite material behavior wherein the material is assumed homogeneous and the effects of the constituent materials are detected only as averaged apparent properties of the composite material.
MDPN452Dr. Mohammad Tawfik
Definitions
• Micromechanics: The study of composite material behavior wherein the interaction of the constituent materials is examined in detail as part of the definition of the behavior of the heterogeneous composite material.
MDPN452Dr. Mohammad Tawfik
Approaches to Micromechanics
• Mechanics of Materials• Elasticity
MDPN452Dr. Mohammad Tawfik
Micromechanics Objective
• To answer the questions set by micromechanics, the objective becomes:
– Determine the elastic moduli or stiffness or compliances of a composite material in terms of the elastic moduli of the constituent materials
( )mimfifii VPVPPP ,,,=
MDPN452Dr. Mohammad Tawfik
Micromechanics Objective
( )mimfifii VPVPPP ,,,=
MaterialCompositeofVolume
FibresofVolumeV f =
fm VV −= 1
MDPN452Dr. Mohammad Tawfik
Basic Assumptions
• The lamina:– Initially stress-free, macroscopically homogeneous,
linearly elastic, macroscopically orthotropic
• The fibers:– Homogeneous, regularly spaced, linearly elastic,
perfectly aligned, Isotropic, perfectly bonded
• The matrix:– Homogeneous, Isotropic, linearly elastic, void-free
MDPN452Dr. Mohammad Tawfik
Representative Volume
• The smallest region or piece of material over which the stresses and strains can be regarded as macroscopically uniform and yet the volume still has the correct proportions of fiber and matrix
MDPN452Dr. Mohammad Tawfik
Mechanics of Materials Approach
MDPN452Dr. Mohammad Tawfik
Most Prominent Assumptions
• In fibre direction, strain in fibres and matrix are equal
• Normal to fibre direction, stresses in matric and fibre are equal
MDPN452Dr. Mohammad Tawfik
Determination of E1
Rule of Mixture
MDPN452Dr. Mohammad Tawfik
Rule of Mixture
MDPN452Dr. Mohammad Tawfik
Experimental Results
MDPN452Dr. Mohammad Tawfik
Determination of E2
MDPN452Dr. Mohammad Tawfik
Determination of E2
• Nondimensionalizing:
MDPN452Dr. Mohammad Tawfik
Experimental Results
MDPN452Dr. Mohammad Tawfik
Determination of Poisson’s Ratio
• We have two values for the Poisson’s Ratio ν12 & ν21.
MDPN452Dr. Mohammad Tawfik
Determination of G12
MDPN452Dr. Mohammad Tawfik
Determination of G12
MDPN452Dr. Mohammad Tawfik
Strength
MDPN452Dr. Mohammad Tawfik
Strength
• “A chain is as strong as its weakest link”• When the composite material gets loaded,
all its components get loaded with different stresses
• Nevertheless, strength prediction of the composite materials have not yet reached the accuracy level of the stiffness prediction. i.e. Open research area!
MDPN452Dr. Mohammad Tawfik
Longitudinal Tensile Strength
• Main assumptions:– All fibres have the same strength– Fibres and matrix behave linearly – Fibres are brittle when compared to matrix– Fibres are stiffer than matrix
MDPN452Dr. Mohammad Tawfik
Longitudinal Tensile Strength
• The stress that will cause the fibres to fail:
• Where is the stress in the matrix as the fibres reach their ultimate stress.
• From that:
mmffut VV *1 σσσ +=
f
mfum E
Eσσ =*
+= m
f
mffut VE
EVσσ 1
MDPN452Dr. Mohammad Tawfik
Longitudinal Tensile Strength
MDPN452Dr. Mohammad Tawfik
Longitudinal Tensile Strength
MDPN452Dr. Mohammad Tawfik
Minimum and Critical Vf
• From the graphs, and using the previous equations, we may calculate:
*
*
mfu
mmucriticalfV σσ
σσ−−=−
*
*
maxmmufu
mmufV σσσ
σσ−+
−=
MDPN452Dr. Mohammad Tawfik
Longitudinal Compressive Strength
• In compression, the failure is dominated by buckling of the fibres!
• Long fibres that are supported by softer matrix material tend to buckle causing what is called Microbuckling
• Microbuckling causes great reduction in the compression stiffness of the composite material
MDPN452Dr. Mohammad Tawfik
MDPN452Dr. Mohammad Tawfik
MDPN452Dr. Mohammad Tawfik
Compressive Strength
• The compressive strength is greatly affected by:
– Buckling modes– Initial misalignment– Curing procedure
MDPN452Dr. Mohammad Tawfik
MDPN452Dr. Mohammad Tawfik
Homework #3
• Read the papers provided to you• Read section 4.4 in textbook• Collect more papers evolving the same topics (at
least 3 per topic)• Write down a report on each topic• Due dates:
– Tensile Failure; axial and transverse– Compressive failure ; axial and transverse
(19/10/2013 23:59)
MDPN452Dr. Mohammad Tawfik
Report should include
1. Introduction to the topic (need, problems, history, etc...)
2. Models available in literature (Including the detailed derivation of at least one of the models)
3. Results obtained from different models compared to experimental results (direct from available literature)
4. Conclusions about the models and their accuracy
5. References and bibliography