MMComposites_NTKien
description
Transcript of MMComposites_NTKien
Faculty of Civil Engineering and Applied Mechanics
Department of Structures
Mechanics of Composite Materials
� PhD. Nguyễn Trung KiênEmail: [email protected] of Civil Engineering and Applied Mechanics1 Vo Van Ngan Street, Thu Duc DistrictHo Chi Minh City, Viet Nam
� Keywords: - Mechanics of Composite Materials- Laminated materials and Structures- Homogenization- Theory of plates and beams
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
2
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
References
� Autar K. Kaw, Mechanics of Composite Materials, Taylor & Francis, NewYork, 2006
� Jean-Marie Berthelot, Composite Materials –
3
� Jean-Marie Berthelot, Composite Materials –Mechanical behavior and Structural analysis, Springer, 1999
� J. N. Reddy, Mechanics of laminated composite plates and shells – Theory and Analysis, CRC Press, 2004. Press, 2004.
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
4
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
INTRODUCTION TO COMPOSITE MATERIALS
� Introduction
� Composite materialsMatrix materials
5
o Matrix materialso Fiberso Architecture of composite materials
o Study the mechanical behavior of composite materials
� Composite materials for civil engineering applications� Composite materials for civil engineering applications
Introduction
� Composite materials used more and more for primary structures in aerospace, marine, energy,…
6
Introduction
� Composite materials used more and more for primary structures in civil engineering, etc
7
Composite materials
� Definition:
o “Composite” means "made of two or more different parts
� Classification:
8
� Classification:o Form of constituents
� Fiber composite� Particle composite
o Nature of Constituents� Organic matrix composites� Metallic matrix composites� Metallic matrix composites� Mineral matrix composites
Composite materials
� Classification by class of constituents
9
Fiber Reinforcement Matrix Composite
Particle Matrix CompositeParticle Matrix Composite
� Mechanical properties of composites� the nature of the constituents� the proportions of the constituents� the orientation of the fibers
Composite materials
� Matrix comprises a resin (polyester, epoxide, etc.) and fillers which is to improve the characteristics of the resin:o Thermosetting Resins:
10
o Thermosetting Resins: � Polyester Resins
� Condensation Resins � Epoxide Resins
o Thermoplastic Resins: � polyvinyl chloride (PVC), polyethylene, polypropylene, polystirene,
polyamide, and polycarbonate
o Thermostable Resins: o Thermostable Resins: o Bismaleimide Resins, Polyimide Resins
Composite materials
� Epoxide Resins:
11
Advantages of epoxide resins are the following:� good mechanical properties (tension, bending, compression, shock, etc.) superior to those of polyesters� good behavior at high temperatures: up to 150-190°C in continuous use� excellent chemical resistance� low shrinkage in molding process and during cure (from 0.5-1 %)� very good wettability of reinforcements� excellent adhesion to metallic materials
Disadvantages:� High cost, manufacture, sensibility to cracking
Composite materials
� Polypropylene, polyamide:
12
Advantages of epoxide resins are the following:� low cost, fabrication
Disadvantages:� mechanical and thermomechanical properties : low� mechanical and thermomechanical properties : low
���� Limited development
� Thermostable Resins : Bismaleimide Resins, Polyimide Resins
� Thermal performance developed especially in the aviation and space
Composite materials
� Fillers and additives : function of improving the mechanical and physical characteristics of the finished product or making their manufacture easier
� Fillers : Reinforcing Fillers, Nonreinforcing Fillers
13
� Fillers : Reinforcing Fillers, Nonreinforcing Fillerso Reinforcing Fillers : improve the mechanical properties of a resin
� Spherical fillers: diameter usually lying between 10 and 150µm. They can be glass, carbon, or organic (epoxide, phenolic, polystirene, etc.),
� Nonspherical fillers: mica used most (dimension: 100-500µm, thickness: 1-20 µm)
o Nonreinforcing Fillers: reducing the cost of resins, preserving their performance � carbonates, silicates
� Additives : pigments and colorants, antishrinkage agents, antiultraviolet agents
Composite materials
� Fibers:� Improve mechanical characteristics: stiffness,strength, hardness, etc� Improve certain of the physical properties: thermal properties, fire
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� Improve certain of the physical properties: thermal properties, fire resistance, resistance to abrasion, electrical properties
� Reinforcements origins: vegetable, mineral, artificial, synthetic � fibers� linear forms (strands, yarns, rovings, etc.)�surfacing tissues (woven fabrics, mats, etc.)�multidirectional forms (preforms, complex cloths, etc.)
Composite materials
� Specific mechanical characteristics of materials, made in the form of fibers
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Composite materials
� Architecture of composite materials� Laminates
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Composite materials
� Architecture of composite materialso Sandwich
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Composite materials
� Study the mechanical behavior of composite materials
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Composite materials
� Study the mechanical behavior of composite materials
19
Composite materials for civil engineering applications
20
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
21
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
MECHANICAL BEHAVIORS OF COMPOSITE MATERIALS
� Linear elastic scheme
� Elastic behavior of a unidirectional composite material� Elastic behavior of an orthotropic composite material
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� Elastic behavior of an orthotropic composite material� Elastic behavior of composite materials outside of main
axes� Strength failure theories
Mechanical behaviors of composite materials
� Linear elastic scheme
o Stiffness and compliance matrix
σ ε
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11 12 13 14 15 161 1
12 22 23 24 25 262 2
13 23 33 34 35 363 3
14 24 34 44 45 4623 23
15 25 35 45 55 5613 13
16 26 36 46 56 6612 12
C C C C C C
C C C C C C
C C C C C C
C C C C C C
C C C C C C
C C C C C C
σ εσ εσ εσ γσ γσ γ
=
ε σ11 12 13 14 15 161 1
12 22 23 24 25 262 2
13 23 33 34 35 363 3
14 24 34 44 45 4623 23
15 25 35 45 55 5613 13
16 26 36 46 56 6612 12
S S S S S S
S S S S S S
S S S S S S
S S S S S S
S S S S S S
S S S S S S
ε σε σε σγ σγ σγ σ
=
� C, S 6x6-matrix is called the stiffness matrix and compliance matrix having 21 independent constants: S = C-1
Mechanical behaviors of composite materials
� Change of coordinate system
, = =σ Cε ε Sσ
� Vector:
24
where
� Tensor:
Rotation of a ɵ angle of coordinate system around 3-axis
Mechanical behaviors of composite materials
� Change of coordinate system
, = =σ Cε ε Sσ
� Stress:
25
� In coordinate system e: σ = C ε� In coordinate system e': σ’ = C’ ε’
1' −=C T CTwhere :
Rotation of a ɵ angle of coordinate system around 3-axis
1' −=σ ε
C T CTwhere :
( )1
' , '
−
= =
=
σ ε
ε σ
σ T σ ε T ε
T TT
� Stresses and strains in e’:
Mechanical behaviors of composite materials
� Change of coordinate system
, = =σ Cε ε Sσ
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2 2
2 2
2 2
cos sin 0 0 0 2sin cos
sin cos 0 0 0 2sin cos
0 0 1 0 0 0
0 0 0 cos sin 0
0 0 0 sin cos 0
sin cos sin cos 0 0 0 cos sin
θ θ θ θθ θ θ θ
θ θθ θ
θ θ θ θ θ θ
−
= −
− −
σT
2 2
2 2
2 2
cos sin 0 0 0 sin cos
sin cos 0 0 0 sin cos
0 0 1 0 0 0
0 0 0 cos sin 0
0 0 0 sin cos 0
2sin cos 2sin cos 0 0 0 cos sin
θ θ θ θθ θ θ θ
θ θθ θ
θ θ θ θ θ θ
−
= −
− −
εT
( )1
' , '
−
= =
=
σ ε
ε σ
σ T σ ε T ε
T TT
� Stresses and strains in e’:
Mechanical behaviors of composite materials
� Engineering Matrix Notation
, = =σ Cε ε Sσ
� Stress:
27
� Strains:
Mechanical behaviors of composite materials
� Anisotropic materials
11 12 13 14 15 161 1C C C C C C
C C C C C C
σ εσ ε
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12 22 23 24 25 262 2
13 23 33 34 35 363 3
14 24 34 44 45 4623 23
15 25 35 45 55 5613 13
16 26 36 46 56 6612 12
C C C C C C
C C C C C C
C C C C C C
C C C C C C
C C C C C C
σ εσ εσ γσ γσ γ
=
� Matrix C: 21 independent constants at a pointat a point� Note that these constants can vary from point to point if the material is nonhomogeneous
Mechanical behaviors of composite materials
� Monoclinic material
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1–2 symmetry plane of a monoclinic material
Note:� A monoclinic material is a material that has a symmetry plane� 13 independent elastic constants
Mechanical behaviors of composite materials
� Orthotropic material
30
Note:� Three mutually perpendicular planes of material symmetry� 9 independent elastic constants
Mechanical behaviors of composite materials
� Transverse isotropic material (Unidirectional material)
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Note:� Orthotropic material having one axis of revolution � 5 independent elastic constants
Mechanical behaviors of composite materials
� Isotropic material
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Note:� Properties are independent of the choice of its reference axis� 2 independent elastic constants
Mechanical behaviors of composite materials
� Isotropic material
33
Relations between elasticity coefficients of an isotropic material
� Elasticity modulus: E, νo Uniaxial Tension or Compression
Mechanical behaviors of composite materials
� Exercise 1: In the case of a monoclinic material with the symmetry plane (1,2) show that the stiffness matrix has the form (a).
34
(a) (b)
� Exercise 2: The symmetry plane (1,3) is added to a monoclinic material in order to obtain an orthotropic material. Show that the stiffness matrix has the form (b)
(a) (b)
C2 – Mechanical behaviors of composite materials
� Exercises 3: Consider a rotation through an angle e about the I-axis of an orthotropic material. Write the stiffness matrix in the new axes and deduce the form (a) of the stiffness matrix of a transverse isotropic material.
35
isotropic material.
� Exercise 4: In case of isotropic material, show that the stiffness matrix has the form (b)
(a) (b)
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
36
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
ELASTIC BEHAVIOR OF UNIDIRECTIONAL COMPOSITE MATERIALS
� Effective moduli:
37
� Microscopic scale : scale of constituents.
Microscopic ↔ Macroscopic
� Macroscopic scale of size δ : properties of the material can be averaged to agood approximation. The properties measured in a sample of size δ areindependent of the place (of the point)� Homogenized problems of designing structures can be solved by considering theaverage properties measured on the scale δ.� Macroscopic homogeneity or statistical homogeneity � Homogenization.
Effective properties of composites
�How to determine the homogenized properties� Phenomenological approach� Homogenization method
38
� Homogenization method
Homogenization method Phenomenological method
Effective properties of composites
� An element of volume V and size δ:
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Basic equations of the average strain and stress field:
� C: Effective stiffness matrix� S: Effective compliance matrix
Homogenization of composite materials
�Homogenization method: 3 main stages• Representative Volume Element (RVE)• Localization problem
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• Localization problem • Homogenization
Periodic materials Random materials
Periodic material media
� Localization problem of periodic composites
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� Strain energy:
� Macroscopic constitutive equation:
� Resolution method of the elastic problem on a unit cell: FEM, Fourier(Gusev, Kanit et al., Suquet et al., Mishneavsky, etc)
� Strain energy:
Elastic behavior of unidirectional composite
�Unidirectional composite material
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L: Longitudinal direction T, T’: Transverse direction
� Hook’s law: � 5 independent coefficients: � 5 independent coefficients: C11, C12, C22, C23, C66
How ?
Engineering constants - Tests
� Engineering constants: Young's moduli (E), Poisson ratios (ν), shear moduli (G).� Longitudinal Tensile Test
43
� Longitudinal Tensile Test
� Stress and strain:
� Elastic moduli:
Engineering constants - Tests
� Transverse tensile test
44
� Stress and strain:
� Elastic moduli:
(ν21)
(ν23)
Nota:
Engineering constants - Tests
� Longitudinal shear test � Transverse shear test
45
� Stress and strain:
� Elastic moduli:
� Stress and strain:
� Elastic moduli:
Nota:
(G23)
Engineering constants - Tests
�Lateral hydrostatic compression
46
� Stress and strain:
� Lateral compression modulus:
Engineering constants - Tests
� Moduli as functions of the stiffness
47
� Only 5 independent moduli, practically: E , E , νννν , G , G� Only 5 independent moduli, practically: EL, ET, ννννLT, GLT, GTT'
Engineering constants - Tests
� Moduli as functions of the stiffness
48
� Stiffness as functions of Moduli� Stiffness as functions of Moduli
Engineering constants – Theoretical approach
� Different approach to the problem� Find 5 independent constants as functions of the mechanical and
geometric properties of the constituents (engineering constants of
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the matrix and fibers, volume fraction of the fibers),…
� Periodic fiber arrangements:
� Random fiber arrangements:� Random fiber arrangements:
How to estimate elastic constants ?
Engineering constants – Theoretical approach
� Estimation of elastic constants:� Bounds (upper and lower bounds) using energy variational
theorems (total potential energy theorem, Hashin-Shtrikman,…) :
50
not accurate for high contrast of materials
� Exact solutions: simple geometry
� Numerical methods (FEM, Fourier)
Engineering constants – Theoretical approach
� Bounds on engineering constants:� Total potential energy theorem (displacement approach): upper
bounds
51
� Complementary potential energy theorem (stress approach): lower approach
Random fibers Periodic fibers
Engineering constants – Theoretical approach
� Bounds on engineering constants:
52
Engineering constants – Theoretical approach
� Simplified approach:� Longitudinal Young’s modulus:
53
Engineering constants – Theoretical approach
� Transverse Young’s modulus:
54
Engineering constants – Theoretical approach
� Longitudinal Poisson ratio:
55
Engineering constants – Theoretical approach
� Longitudinal shear modulus:
56
Exercises
57
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
58
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
Elastic behavior of orthotropic composite
�Orthotropic composite material� 9 independent coefficients: C11, C12, C13, C22, C23, C33, C44 ,C55, C66
59
� Hook’s law:
C11, C12, C13, C22, C23, C33, C44 ,C55, C66
How ?
S11, S12, S13, S22, S23, S33, S44 , S55, S66
Elastic behavior of orthotropic composite
�Orthotropic composite material
60
C11, C12, C13, C22, C23, C44 ,C55, C66
S , S , S , S , S , S , S , SS11, S12, S13, S22, S23, S44 , S55, S66
Engineering constants - Tests
� Engineering constants: Young's moduli (E), Poisson ratios (ν), shear moduli (G).� Tensile test in direction 1
61
� Tensile test in direction 1
� Tensile test in direction 2
� Tensile test in direction 3
Engineering constants - Tests
� Shear test
62
Similarly,
Conclusion:
Engineering constants - Tests
� Compliance constants:
63
� Stiffness constants:
Engineering constants – orthotropic composite
Exercise 1: Calculate the stiffness and compliance constants of an orthotropic composite with the following characteristics:
64
Exercise 2: Calculate the stiffness and compliance constants of an orthotropic composite with the following characteristics:
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
65
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
Off-axis behavior of composite materials
� Constitutive equations of off-axis layers
66
1, 2, 3: principal directions1’, 2’, 3’: reference system
Stiffness and compliance constants:
Off-axis behavior of composite materials
� Elastic constants
67
Off-axis behavior of composite materials
� Exercise: o Determine elastic constants of an orthotropic material whose principal direction 1 makes an angle ɵ with the x-axis directiono Plot the variation of C’11 and C’12 in terms of ɵ (0 - 90o)
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11 12
Two dimensional stress state
� Plane stress state:
69
Two dimensional stress state
� Plane stress state:
70
wherewhere
Q: reduced stiffness matrix
Two dimensional stress state
� Plane stress state in principal directions:
71
Two dimensional stress state
� Plane stress state in off-axis:
72
Two dimensional stress state
� Exercise:
� Consider a plane stress state, determine:- Stresses: σxx, σyy, σxy
73
- Stresses: σxx, σyy, σxy- Stresses in principal axes (L, T)
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
74
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
Fracture and Damage of Composite Materials
� Fracture Processes Induced in Composite Materials :
75
Fracture and Damage of Composite Materials
� Failure Criteria:� Maximum stress criterion
76
+ Xt, Xc: the tensile and compressive strengths in the longitudinal direction+ Yt , Yc: the tensile and compressive strengths in the transverse direction+ S: the in-plane shear strength of the layer
Fracture and Damage of Composite Materials
� Failure Criteria:� Maximum strain criterion
77
+ Xεt, Xεc: the tensile and compressive strains in the longitudinal direction+ Yεt , Yεc: the tensile and compressive strains in the transverse direction+ S: the in-plane shear strain of the layer
Fracture and Damage of Composite Materials
� Failure Criteria:� Interactive criteria
Hill’s criterion:
78
Tsai - Hill’s criterion: plane stress state
Hoffman’s criterion:
Tsai - Wsu criterion: (book)
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
79
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of �C7 : Modeling of mechanical behaviors of
laminated plates�C8 : Homogenization of composite materials
Modeling the Mechanical Behavior of Laminated Plates
� Basics of Laminate Theory :
80
Plate element Laminated element
� Equivalent single-layer theories (2D) � Classical laminate theory � Shear deformation laminate theories
� Three-dimensional elasticity theory � 3D elasticity formulations � Layerwise theories
Modeling the Mechanical Behavior of Laminated Plates
� Laminate Theories :
81
Laminated element
Functions to be determined
Various plate theories
Plate models
� Plate model of Love-Kirchhoff:
82
Plate models
� Plate model of Reissner-Mindlin: First-order shear deformation theory
83
Plate models
� High-Order Shear Deformation Plate Model� In-plane displacements varied in the thickness:
84
TSDT :
SSDT : SSDT :
� Transverse displacement varied in the thickness:
Plate models
� Strains and stress
85
� Stress at point of kth-layer:
Plate models
� 2D plate theories� Assumption: σzz=0
86
Plate models
� Resultants and Moments:
87
Plate models
� Resultants and Moments:
88
Classical laminated plate theory
� Hypothesis� Straight lines perpendicular to
the midsurface before
89
the midsurface beforedeformation remain straightafter deformation
� Transverse normals are inextensible
� Transverse normals rotatesuch that they remainperpendicular to theperpendicular to themidsurface after deformation
0, 0zz xz yzε γ γ⇒ = = =
Classical laminated plate theory
� Kinematics
90
� Strains:
Classical laminated plate theory
� Constitutive relations
91
Classical laminated plate theory
� Constitutive relations� A : extensional stiffness� D: bending stiffness
92
� D: bending stiffness� B: bending-extensional coupling stiffness
Classical laminated plate theory
� Constitutive relations� A, B, D : extensional stiffness, bending stiffness, bending-extensional coupling stiffness
93
coupling stiffness
Classical laminated plate theory
� Equations of motion� Governing equations derived using the principle of virtual
displacements
94
displacements
where δU, δV, δK are virtual strain energy, virtual work done and virtual kinetic energy
Classical laminated plate theory
� Equations of motion
95
where
Classical laminated plate theory
� Equations of motion
(1)ε κ
� Note:
96
(1)
(1)
(1)
xx xx
yy yy
xy xy
ε κε κγ κ
=
Classical laminated plate theory
� Equations of motion
97
� Equilibrium equation:
Classical laminated plate theory
� Equations of motion
98
Classical laminated plate theory
� Equations of motion
99
Classical laminated plate theory
� Equations of motion
100
First-order shear deformation laminated plate theory
� Hypothesis� Straight lines perpendicular to
the midsurface before
101
the midsurface beforedeformation remain straightafter deformation
� Transverse normals are inextensible
� Kinematics
� Exercise: Equations of motion ?� Shear correction factor : k=5/6
Laminated plate theory
�Laminate stiffnesses� Angle-ply laminates, cross-ply laminates
102
General angle-ply laminate Cross-ply laminate
� General angle-ply laminate:ɵ and - ɵ orientation in [0,90]
� Cross-ply laminate:ɵ orientation of 0o or 90o
Laminated plate theory
�Laminate stiffnesses� Symmetric and asymmetric laminates
103
� Notation : (-25/35/0/90)s
�Laminate stiffnesses� Material stiffnesses, layer thicknesses, lamination scheme
Laminated plate theory
�Laminate stiffnesses� Isotropic layers
104
Examples: � Single isotropic layer� Single orthotropic layer
Analytical solution
�Navier solution
105
Analytical solution
�Characteristic equations
106
Analytical solution
� Bending analysis
107
� Buckling analysis
� Free vibration
Contents
�C1 : Introduction to composite materials�C2 : Mechanical behaviors of composite materials�C3 : Elastic behavior of unidirectional composite
108
�C3 : Elastic behavior of unidirectional composite materials
�C4 : Elastic behavior of orthotropic composite�C5 : Off-axis behavior of composite materials�C6 : Fracture and damage of composite materials�C7 : Modeling of mechanical behaviors of laminated �C7 : Modeling of mechanical behaviors of laminated
plates�C8 : Homogenization of composite materials
Homogenization of composite materials
� Introduction:
109
� Material can be considered to be homogeneous or heterogeneous according tothe scale at which it is observed.
Microscopic ↔ Macroscopic
Homogenization
the scale at which it is observed.
� Material can be described in the framework of continuum mechanics by twomodels: one at microscopic scale where the behavior is heterogeneous, the otherat macroscopic scale where the behavior is homogeneous.
� Objective of homogenization: study the relation of these two models, especiallydetermination of behavior at macroscopic scale in terms of one at microscopicscale.
Homogenization of composite materials
� Introduction:
110
� Determination of behavior at macroscopic scale in terms of one at microscopicscale:
� Representative volume element (RVE) whose boundary subjected to
HomogenizationPhenomenological method
� Representative volume element (RVE) whose boundary subjected tohomogeneous boundary conditions in strain and stress.
� Macroscopic behavior is the relation between volume average of stress andstrain in RVE
� Size of RVE should be large enough at micro scale to well describeheterogeneity, and small enough at macro scale in which calculatedmechanical fields are very few variables in RVE
Homogenization of composite materials
� Introduction:
111
� Scale of structure: macroscopic scale
Heterogeneity scale RVE scale
� Scale of structure: macroscopic scale
� Scale of heterogeneity : microscopic scale
� Scale of RVE: mesoscopic scale
� Concept of RVE: linear elasticity, nonlinear elasticity, elastoplasticity, limitanalysis
Homogenization of composite materials
� Objective:
� Definition of homogenized linear elasticproperties of heterogeneous materials
112
properties of heterogeneous materials
� Presentation of bounds that enable toestimate the properties in terms ofconstituent properties
� Hypothesis:� Small deformation
� Heterogeneous linear elastic materials
� No cavities, cracks
� Constituents are perfectly adherent
Homogenization of composite materials
� Average value on RVE:
( )1D
f f dVV ∈
= ∫x V
xDefinition:
113
V ∈∫
x V
( ) ( ){ }0
0
0 in , . .
V
div= = =
⇒ =
σ x σ x V σ n σ n
σ σ
� Average of stress :
Homogenization of composite materials
� Average of strain on RVE:
Consider : ( ) ( ) ( ) ( ) 00
1, . on V
2t= ∇ + ∇ = = ∂ε x u u u x u x ε x
114
Average strain field of RVE:
Homogenization of composite materials
� Average value on RVE:
( )1 1 . . .dV dS= =∫ ∫σ ε σε u σ n
� Homogeneous boundary condition in stress:
115
( ) . . .
, . . . .
VV
V
V V V
dV dSV V
V
∈ ∈∂
= =
=∀ ∈∂ = ⇒ =
∫ ∫x D x
σ ε σε u σ n
σ Σ
x σ n Σnσ ε σ ε
� Homogeneous boundary condition in strain:
( ), . VV =∀ ∈∂ = ⇒ ε E
x u x E x( ), . . .V
V V V
V =∀ ∈∂ = ⇒
=
ε Ex u x E x
σ ε σ ε
� Hill – Mandel’s principle :
. .V V V
=σ ε σ ε
Homogenization of composite materials
� Homogenization with strain approach:( ) . V= ∈∂u x E x x AV∈ V and BCs �Direct method:
116
Heterogeneous : a(x) Homogeneous : A
( )� Elastic problem on RVE: solutions (σE, εE, uE) � Nota :
A ? for a (x)
E VV∀ ⇒ = =E Σ σ A E
( )( ) ( ) ( )
( ) ( )( )
0
1
2.
t
div
V
=
=
= ∇ + ∇
= ∈∂
σ x
σ x a x ε x
ε x u u
u x E x x
( )( )( )( )
, if ,
,
.
E
E
E
V
V
∀ ∈ =
=
⇒∀ ∈ = =
x a x A
σ x AE
x ε x E
u x E x
� E : uniform strain in RVE
. .E E E EV V V= =σ ε σ ε ΣE
Homogenization of composite materials
� Potential energy method
( ) ( ) ( ) ( )( ): .
E E KAW Min W
KA V
∈− Φ = − Φ
∈ = ∈∂uu u u u
u u x E x x
117
( )
( ) ( ) ( ) ( ) ( )
: .
1. . , 0
2
KA V
W dV∈
∈ = ∈∂
= Φ =∫x D
u u x E x x
u ε x a x ε x u
Minimum principle of potential energy:
( ) ( ) ( )( ) ( )
. 0 V= + ⇒ = ∀ ∈ ∂
= +
u x u x E x u x x
ε x ε u E
ɶ ɶ
ɶ
( )( ) ( ) ( )( ) ( )( ) ( ) ( )( )( ) ( ) ( ) ( )( )
( )( ) ( ) ( )( )
( )( ) ( ) ( )( )
. . . .
,
. .
, . .
E E KAV V
E E E E
E E E E E E VV V VV
V KA V
Min
Min
∈
∈
+ + = + +
= + = +
+ + = = =
⇒∀ = + +
u
u
ε u E a x ε u E ε u E a x ε u E
ε u ε u E σ a x ε u E
ε u E a x ε u E σ ε σ ε EA E
E EA E ε u E a x ε u E
ɶ ɶ ɶ ɶ
ɶ ɶ
ɶ ɶ
ɶ ɶ
Homogenization of composite materials
� Complementary energy method
( ) ( ) ( ) ( ),
: 0
E E SAW Min W
SA div
∈∀ − Φ = − Φ
∈ =σ
E σ σ σ σ
σ σ
118
( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )
: 0
1. . , . . .
2 V V
SA div
W dV dS dV∈ ∈∂ ∈
∈ =
= Φ = =∫ ∫ ∫x D x x
σ σ
σ σ x s x σ x u E x σ n E σ x
( ) ( )( )
. . 2 . . 2
. .
E E E SAV VV V
E E E E E E VV V VV
Min ∈ − = −
= = =
σσ s x σ E σ σ s x σ E σ
σ s x σ σ ε σ ε EA E
Minimum principle of complementary energy:
( ), 2 . .V SA V VMax ∈
⇒∀ = − σE EA E E σ σ s x σ
Conclusions:
( ) ( )( ) ( ) ( )( ), 2 . . . .SA V KAV V VMax Min∈ ∈
∀ − = = + + σ uE E σ σ s x σ EA E ε u E a x ε u Eɶ ɶ
Homogenization of composite materials
� Homogenization with stress approach:
( ) V= ∈∂σ x n Σn x�Direct method:
119
( ) 0 div =σ x
� Elastic problem on RVE: solutions (σ∑, ε ∑, u ∑):
Heterogeneous : s(x) Homogeneous : S
( ): 0, SA div V∈ = = ∈∂σ σ σ x n Σn x( )
( ) ( ) ( )
( ) ( )( )
0
1
2
t
div
V
=
=
= ∇ + ∇
= ∈∂
σ x
σ x a x ε x
ε x u u
σ x n Σn x
VVΣ =ε S Σ
( ) ( ) ( ) ( ) ( ) ( ) ( ), 2 . . . .V SAV V VMax Min ∈
∀ − = = + + u σΣ Σ ε u ε u a x ε u ΣS Σ σ Σ s x σ Σɶ ɶ
Homogenization of composite materials
� Homogenized properties of a heterogeneous medium:
120
Homogenization of composite materials
� Bounds on Ahom:
� Voigt and Reuss
121
( ), V Vf aα α
α
∀ ≤ = ∑E EA E E a x E E E
( ) ( )( ) ( ) ( )( ), 2 . . . .SA V KAV V VMax Min∈ ∈
∀ − = = + + σ uE E σ σ s x σ EA E ε u E a x ε u Eɶ ɶ
(Voigt’s bound)
1f α −
( )( )
0 0 0 0
1
1
hom
, 2
,
,
VV
VV
f sα α
α
−
−
∀ − ≤
⇒∀ ≤
⇒∀ ≤
∑
E σ Eσ σ s x σ EA E
E E s x E EA E
E E E EA E
(Reuss’s bound)
1
hom
1
hom
9 3 2,
3 6 2
fK f K
K
ff
K KE
K K
αα α
αα α
αα α
αα α
µ µµ
µ µνµ µ
−
−
≤ ≤
≤ ≤
−= =+ +
∑ ∑
∑ ∑
Homogenization of composite materials
� Bounds on Ahom:
� Hashin-Shtrikman
K K V Vµ µ− −− −
122
( ) ( )
( ) ( )
( ) ( )
1 2 1 2
2 1 2 12 1 2 12 2
1 1 1 1
1 2 1 2
2 1 2 12 1 2 12 2
1 2 1 2
;1 1 1 1
4 / 3
;1 1 1 1
4 / 3
9 8 / 6 2
9 3 2
K K V VK KK K V V
K f
K K V VK KK K V V
K f
f K K
K Kα α α α α α
µ µµ µµ µ
µ µµ µ
µ µµ µµ µ
µ µ µµ µ
− −
+ +
− −= =− −− −+ − + −+ +
− −= =− −− −+ − + −+ +
= + +−
2 1 2 1
9 3 2,
3 6 2
: ,
K KE
K K
Nota K K
µ µνµ µ
µ µ
−= =+ +
≥ ≥