chapter 3 micromechanical analysis of a...

55
Chapter 3 Micromechanical Analysis of a Lamina Elastic Moduli Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa, FL 33620 Courtesy of the Textbook Mechanics of Composite Materials by Kaw

Upload: trinhkien

Post on 15-Oct-2018

224 views

Category:

Documents


1 download

TRANSCRIPT

Page 1: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Chapter 3 Micromechanical Analysis of a LaminaElastic Moduli

Dr. Autar KawDepartment of Mechanical Engineering

University of South Florida, Tampa, FL 33620

Courtesy of the TextbookMechanics of Composite Materials by Kaw

Page 2: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

h, t = A ff

and h, t = A mm

ht = A cc

Page 3: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

tt =

AA = V

c

f

c

ff

V - 1 =tt =

AA = V

f

c

m

c

mm

Page 4: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

1

2 3

h

tc

tm/2 tf

tm/2

h

tc

Lc

FIGURE 3.3Representative volume element of a unidirectional lamina.

Page 5: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

h

tc tm/2

tf tm/2

σc σc

FIGURE 3.4A longitudinal stress applied to the representative volume element to calculate the longitudinal Young’s modulus for a unidirectional lamina.

Page 6: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

,A = F ccc σand ,A = F fff σ

A = F mmm σ

, E = c1c εσand , E = fff εσ

εσ mmm E =

F + F = F mfc

Page 7: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

A E + A E = A E mmmfffcc1 εεε

: then),( If εεε mfc = =

AA E +

A

A E = E

c

mm

c

ff1 V E + V E = E mmff1

Page 8: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

V E + V E = E mmff1

V EE =

FF

f1

f

c

f

,A = F ccc σand ,A = F fff σ

A = F mmm σ

, E = c1c εσand , E = fff εσ

εσ mmm E =

Page 9: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

FIGURE 3.5Fraction of load of composite carried by fibers as a function of fiber volume fraction for constant fiber to matrix moduli ratio.

Page 10: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.3

Find the longitudinal elastic modulus of a unidirectional Glass/Epoxy lamina with a 70% fiber volume fraction. Use the properties of glass and epoxy from Tables 3.1 and 3.2, respectively. Also, find the ratio of the load taken by the fibers to that of the composite.

Page 11: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.3

Ef = 85 Gpa

Em = 3.4 GPa

GPa 60.52 =0.3 3.4 + 0.7 85 = E1 )()()()(

Page 12: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.3

FIGURE 3.6Longitudinal Young’s modulus as function of fiber volume fraction and comparison with experimental data points for a typical glass/polyester lamina.

Page 13: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.3

0.9831 = 0.7 60.52

85 = FF

c

f )(

Page 14: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

h

tc

tm/2 tf

tm/2 σc

σc

FIGURE 3.7A transverse stress applied to a representative volume element used to calculate transverse Young’s modulus of a unidirectional lamina.

Page 15: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

σσσ mfc = =

∆∆∆∴ mfc + =

, t = ccc ε∆

and , t = fff ε∆

mmm t = ε∆

,

E = c

c2

σε

and ,E

= f

ff

σε

E =

m

mm

σε

Page 16: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

andtt

E1 +

tt

E1 =

E1

c

m

mc

f

f,

2

EV +

EV =

E1

m

m

f

f

2

Page 17: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.4

Find the transverse Young's modulus of a Glass/Epoxy lamina with a fiber volume fraction of 70%. Use the properties of glass and epoxy from Tables 3.1 and 3.2, respectively.

Page 18: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.4

= 85 GPaE f

Em = 3.4 GPa

GPa 10.37 = E

3.40.3 +

850.7 =

E1

2

2

Page 19: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

FIGURE 3.8Transverse Young’s modulus as a function of fiber volume fraction for constant fiber to matrix moduli ratio.

Page 20: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

πV4

= sd f 2

1

πV32

= sd f

21

Page 21: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

s

d

(b)

(a)

s

d

FIGURE 3.9Fiber to fiber spacing in (a) square packing geometry and (b) hexagonal packing geometry.

Page 22: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

FIGURE 3.10 Theoretical values of transverse Young’s modulus as a function of fiber volume fraction for a boron/epoxy unidirectional lamina (Ef = 414 GPa, vf = 0.2, Em = 4.14 GPa, vm = 0.35) and comparison with experimental values. Figure (b) zooms figure (a) for fiber volume fraction between 0.45 and 0.75. (Experimental data from Hashin, Z., NASA tech. rep. contract no. NAS1-8818, November 1970.)

Page 23: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

h

tc

tm/2 tf

tm/2

σ1 σ1

(b)

(a)

tc

tm/2

tf

tm/2

tc + δcT

Lc

tf + δfT

h

tc

tm/2 tf

tm/2

σ1 σ1

(b)

(a)

tc

tm/2

tf

tm/2

tc + δcT

Lc

tf + δfT

FIGURE 3.11A longitudinal stress applied to a representative volume element to calculate Poisson’s ratio of unidirectional lamina.

Page 24: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

δδδ Tm

Tf

Tc + =

,t

= f

TfT

ε

and ,t

= m

TmT

mδε

t =

c

TcT

cδε

εεε Tmm

Tff

Tcc t + t = t

Page 25: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

,- = L

f

Tf

fεε

ν

and ,- = Lm

Tm

mεεν

εεν L

c

Tc

12 - =

ενενεν Lmmm

Lfff

Lc12c t - t- = t-

Page 26: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

ενενεν Lmmm

Lfff

Lc12c t - t- = t-

: then, If εεε Lm

Lf

Lc = =

ννν mmff12c t + t = t

tt +

tt =

c

mm

c

ff12 ννν V + V = mmff12 ννν

Page 27: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.5

Find the Major and Minor Poisson's ratio of a Glass/Epoxy lamina with a 70% fiber volume fraction. Use the properties of glass and epoxy from Tables 3.1 and 3.2, respectively.

Page 28: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.5

0.2 = fν

0.3 = mν

0.230 = 0.3 0.3 + 0.7 0.2 = 12 )()()()(ν

Page 29: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.5

E1 = 60.52 Gpa

E2 = 10.37 GPa

Page 30: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.5

0.03941 = 60.5210.37 0.230 =

EE =

1

21221 νν

Page 31: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

h

tc

tm/2 tf

tm/2 τc

τc

FIGURE 3.12An in-plane shear stress applied to a representative volume element for finding in-plane shear modulus of a unidirectional lamina.

Page 32: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

δδδ mfc + =

,t = ccc γδ

and ,t = fff γδ

mmm t = γδ

Page 33: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

,

G =

12

cc

τγ

and ,G

= f

ff

τγ

G =

m

mm

τγ

,t = ccc γδ

and ,t = fff γδ

mmm t = γδ

δδδ mfc + =

tG

+ t G

= t G

mm

mf

f

fc

12

c τττ

Page 34: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

tG

+ t G

= t G

mm

mf

f

fc

12

c τττ

: then, If τττ mfc = =

tt

G1 +

tt

G1 =

G1

c

m

mc

f

f12

GV +

GV =

G1

m

m

f

f

12

Page 35: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.6

Find the in-plane shear modulus of a Glass/Epoxy lamina with a 70% fiber volume fraction. Use properties of glass and epoxy from Tables 3.1 and 3.2, respectively.

Page 36: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.6

GPa 85 = E f 0.2 = fν

GPa 35.42 =

0.2 + 1 285 =

+ 1 2E = G

f

ff

)(

)( ν

Page 37: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.6

GPa 3.4 = Em 0.3 = mν

GPa 1.308 =

0.3 + 1 23.40 =

+ 1 2

E = Gm

mm

)(

)( ν

Page 38: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.6

GPa 4.014 = G

1.3080.30 +

35.420.70 =

G1

12

12

Page 39: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

FIGURE 3.13 Theoretical values of in-plane shear modulus as a function of fiber volume fraction and comparison with experimental values for a unidirectional glass/epoxy lamina (Gf = 30.19 GPa, Gm = 1.83 GPa). Figure (b) zooms figure (a) for fiber volume fraction between 0.45 and 0.75. (Experimental data from Hashin, Z., NASA tech. rep. contract no. NAS1-8818, November 1970.)

Page 40: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

V E + V E = E mmff1

V - 1V + 1

= EE

f

f

m

2

ηηξ

ξη

+ E / E1- E / E =

mf

mf

)()(

Page 41: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.7

Find the transverse Young's modulus for a Glass/Epoxy lamina with a 70% fiber volume fraction. Use the properties for glass and epoxy from Tables 3.1 and 3.2, respectively. Use Halphin-Tsai equations for a circular fiber in a square array packing geometry.

Page 42: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.7

a

b

σ2

σ2

FIGURE 3.14Concept of direction of loading for calculation of transverse Young’s modulus by Halphin–Tsai equations.

Page 43: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.7

2 = ξ Ef = 85 GPa Em = 3.4 GPa

0.8889 =

2 + 85/3.41 - 85/3.4 =

)()(η

Page 44: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.7

GPa 20.20 = E

0.70.8889 10.70.88892+ 1 =

3.4E

2

2

))(())((

Page 45: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

FIGURE 3.15 Theoretical values of transverse Young’s modulus as a function of fiber volume fraction and comparison with experimental values for boron/epoxy unidirectional lamina (Ef = 414 GPa, νf = 0.2, Em = 4.14 GPa, νm = 0.35). Figure (b) zooms figure (a) for fiber volume fraction between 0.45 and 0.75. (Experimental data from Hashin, Z., NASA tech. rep. contract no. NAS1-8818, November 1970.)

Page 46: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Ef/Em = 1 implies = 0, (homogeneous medium)

Ef/Em implies = 1, (rigid inclusions)

Ef/Em implies (voids)

∞→

η

η

0→

ξη 1 - =

Page 47: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

a

b

τ12 τ12

FIGURE 3.16Concept of direction of loading to calculate in-plane shear modulus by Halphin–Tsai equations.

Page 48: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

V + V = mmff12 ννν

V - 1V + 1

= GG

f

f

m

12

ηηξ

ξη

+ G / G1 - G / G =

mf

mf

)()(

V40 + 1 = 10fξ

Page 49: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

Using Halphin-Tsai equations, find the shear modulus of a Glass/Epoxy composite with a 70% fiber volume fraction. Use the properties of glass and epoxy from Tables 3.1 and 3.2, respectively. Assume the fibers are circular and are packed in a square array. Also get the value of the shear modulus by using Hewitt and Malherbe’s8 formula for the reinforcing factor.

Page 50: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

1 = ξ GPa 35.42 = G f GPa 1.308 = Gm

0.9288 =

1 + 835.42/1.301 - 835.42/1.30 =

)()(η

Page 51: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

GPa 6.169 = G

0.7 0.9288 10.7 0.9288 1 + 1 =

1.308G

12

12

)()()()()(

Page 52: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

2.130 =0.7 40 + 1 =

V 40 + 1 = 10

10f

)(

ξ

Page 53: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

0.8928 =2.130 + 1.308 / 35.42

1 - 1.308 / 35.42 = )(

)(η

Page 54: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw

Example 3.8

GPa 8.130 = G

0.7 0.8928 - 10.7 0.8928 2.130 + 1 =

1.308G

12

12

)()()()()(

Page 55: Chapter 3 Micromechanical Analysis of a Laminakaw/compositesOCW/ppts/chapter3_revised/chapter3_3... · Chapter 3 Micromechanical Analysis of a Lamina. Elastic Moduli. Dr. Autar Kaw