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HW (3)
Problem: given that:
is thermal expansion coefficient for fiber
is thermal expansion coefficient for matrix
Calculate: and in for lamina
Solution:
 From hook’s law in 1D stress state, we have two types of
strains:
1. Mechanical strain according to load /Area (σ) is
=
2. Thermal strain according to temperature change ΔT
= α.ΔT
So, we combine thermal and mechanical effects
The total strain = + α.ΔT or σ = E(ϵ – α.ΔT) …….Equ(1)
Where E is the young modulus
σ is the stress
is the strain
 Apply stress σ1 in direction (1) as following:
= = ….. Equ(2)
= . + . ….. Equ(3)
So, from Equ(1) …. = ( – .ΔT) and
= ( – .ΔT)
𝜎 𝜎
= ( – .ΔT)…. Equ(4)
From equations 1,2,3,4:
= . ( – .ΔT) + . ( – .ΔT) or
( – .ΔT) = . ( – .ΔT) + . ( – .ΔT)
So, – .ΔT = . + .
– ΔT.( . + . ) …. Equ(5)
From equations 2,5:
– .ΔT = . + .
– ΔT.( . + . ) …. Equ(6)
From comparison between right side and left side:
= . + .
Or
 Apply stress σ2 in direction (2) as following:
= = ….. Equ(7)
= . + . ….. Equ(8)
𝛼 =
𝑉𝑓 𝐸𝑓 𝛼 𝑓 + 𝑉𝑚 𝐸 𝑚 𝛼 𝑚
𝐸
𝜎
𝜎
From equations 1,8:
+ .ΔT = ( + .ΔT). + ( + .ΔT).
+ .ΔT = + .ΔT + + .ΔT ….Equ(9)
From equations 7,9:
+ .ΔT = + ) + + )
So, 𝛼 = 𝛼 𝑚 𝑉𝑚 + 𝛼 𝑓 𝑉𝑓

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Hw3

  • 1. HW (3) Problem: given that: is thermal expansion coefficient for fiber is thermal expansion coefficient for matrix Calculate: and in for lamina Solution:  From hook’s law in 1D stress state, we have two types of strains: 1. Mechanical strain according to load /Area (σ) is = 2. Thermal strain according to temperature change ΔT = α.ΔT So, we combine thermal and mechanical effects The total strain = + α.ΔT or σ = E(ϵ – α.ΔT) …….Equ(1) Where E is the young modulus σ is the stress is the strain  Apply stress σ1 in direction (1) as following: = = ….. Equ(2) = . + . ….. Equ(3) So, from Equ(1) …. = ( – .ΔT) and = ( – .ΔT) 𝜎 𝜎
  • 2. = ( – .ΔT)…. Equ(4) From equations 1,2,3,4: = . ( – .ΔT) + . ( – .ΔT) or ( – .ΔT) = . ( – .ΔT) + . ( – .ΔT) So, – .ΔT = . + . – ΔT.( . + . ) …. Equ(5) From equations 2,5: – .ΔT = . + . – ΔT.( . + . ) …. Equ(6) From comparison between right side and left side: = . + . Or  Apply stress σ2 in direction (2) as following: = = ….. Equ(7) = . + . ….. Equ(8) 𝛼 = 𝑉𝑓 𝐸𝑓 𝛼 𝑓 + 𝑉𝑚 𝐸 𝑚 𝛼 𝑚 𝐸 𝜎 𝜎
  • 3. From equations 1,8: + .ΔT = ( + .ΔT). + ( + .ΔT). + .ΔT = + .ΔT + + .ΔT ….Equ(9) From equations 7,9: + .ΔT = + ) + + ) So, 𝛼 = 𝛼 𝑚 𝑉𝑚 + 𝛼 𝑓 𝑉𝑓