Strain tensor
Strain tensor can be calculated for any magnitude of strain:
- Ξ = 1/2 [Φ + Φtranspose + ΦtransposeΦ]
- E₁₁ ➔ stretch of fibers directed along direction 1
- E₁₂ ➔ change of angle between direction 1 and 2
For normal strain, we neglect ΦtransposeΦ:
Ξ ≈ Ξ - 1/2 [Φ + Φtranspose] second order term
Ξij = 1/2 (∂Ui/∂Xj + ∂Uj/∂Xi)
X and X are quite the same, so we can deviate with respect to X or X; it's the same.
Numerical example
X1 = X1 + αX1 we only have displacement in direction 1 α > 0
X2 = X2
X3 = X3 ➔ here X2 = 0
Deformation gradient F:
| 1 | α | 0 |
| 0 | 1 | 0 |
| 0 | 0 | 1 |
Strain tensor calculation
ε = 1/2 [Φ + Φtranspose + ΦtransposeΦ] can be calculated for any magnitude of strain:
- E₁₁ ➔ stretch of fibers directed along direction 1
- E₁₂ ➔ change of angle between direction 1 and 2
For normal strain, we neglect ΦtransposeΦ:
ε ➔ ξ - 1/2 [Φ + Φtranspose] second order term
εij = 1/2 (∂ui/∂xj + ∂uj/∂xi)
X and X are quite the same, so we can deviate with respect to x or X; it's the same.
Numerical example
x1 = X1 + αX1 d>0 we only have displacement in direction 1
x2 = X2
x3 = X3 here, ξ2 = 0
Deformation gradient F:
| 1 | α | 0 |
| 0 | 1 | 0 |
| 0 | 0 | 1 |
Green tensor
Green Tensor E:
E = E1 - E = [α01]- [n d 0]...[0 α 0]small strain
Lagrange Strain Tensor E = 1 / 2 (E - I) = 1 / 2[0 α 0] can be neglected because it is small. If α is large, no way we have large strain α2 plays a role.
α2 E22 ➔ no refers to the elongation of those fibers. E44 = 0 ➔ no stretching of fibers along direction α. If we have a biological material with fibers directed in direction Z, they start to play a role when strains are large.
Stress state in large deformations
Now we want to describe the stress state in a material subjected to large deformation before we define the strain rate, which is the derivative of strain components:
σ = ∂U / ∂ε
Elastic energy W(ε) gives us the idea of how much energy we put into a material sample when it is subjected to this strain ε
σ = ∂W / ∂ε
ε̇ strain rate ➔ measures time derivative of strain
ξ = 1/2 ( ∂Mi/∂xj + ∂Mj/∂xi )
DD = 1/2 ( L + LT ) where L = ∂Mi/∂xj velocity gradient
Strain rate in small strain problem: D 2D = ( L+LT )
F → EE = ∂x/∂X so F = ∂E/∂t
∂x/∂X = ∂x/∂XE = FEt - (FT Et) - FT E + ET E = 2FT D
EE = 1/2 C
It comes from ξ = 1/2 ( C - I ), we make the deviate = FT D E
We use these results to define the stress. In large strain problems, we have more than one definition of stress.
σ̇ - ∂W/∂ξ = σ + ∂W/∂ξ
W : energy rate per unit volume
ρW : energy rate per unit mass
x x mean product that ẇ = gives a scalar as result
ρ ẇ = ρ ẇ = σu Du
When we define w(ξ), we need also to define ẇ̇ and then ρ ẇ
From energy considerations, we give other definitions:
ρo is density in current configurations. Now we define ρ in the initial configuration as ρo
ρo ẇ = ρo - ρo ẇ = ρo : D ρ = ρo ρ = ρ o ρ = ρ = ρo = ρo = ∶o ρ o = 0op= dmso ρ ẇ = σ : D : ρ - σ : D :σ ρ σI = I
σ Cauchy stress Kirchhoff Strain Tensor
First Piola-Kirchhoff stress tensor
T oi&suppro;&o;m is a non symmetric stress tensor model for this reason modal for this reason F ⊃ energy based definition of stress
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