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THERMALSTRESS & STRAINS
By
DEEPAK ROTTI
Roll No: 017
KLS’s G.I.T BELGAUM
 Temperature changes occur:
 High speed travelling objects, parts & vehicles.
 Heat engines and rocket engines.
 Boilers, furnace etc.
 Effect of temperature change :
 Mechanical expansion & significance
 Changes in material properties.
 Expansion due to heat: Analogy:
 Strains induced internally.
 Hence stress induced .
Thermal stress effects:
Block of material
subjected to an increase
in temperature
B’
Changes in temperature produce expansion or contraction of
materials and result in thermal strains and thermal stresses
Thermal strain εT is proportional to the temperature change ΔT :
 εT = α (ΔT) (Where α is coefficient of
thermal expansion)
 Sign convention for thermal strains : Expansion is positive and
contraction is negative
Relation between stress (Ϭ) and
change in temperature (ϪT).
• Suppose we have a bar subjected to an axial load.
 ε = σ / E
• Also, we have an identical bar subjected to a temperature change ΔT.
 εT = α (ΔT)
• Equating the above two strains we will get:
 σ = E α (ΔT)
Increase in length of a prismatic
bar due to a uniform increase in
temperature
1
2
3
Thermo-elastic stress &
strain relations:
Fig:A Fig:B
Uniform rise in temperature
(unconstrained)
Hence uniform change in
dimension.
Non-uniform change in
temperature and
hence uneven stress
development
T=T(t, x, y, z)
Total strain = normal strain (αT) + strain due
to stress components
 €x = бx –ν (бy + бz) + Δ α T
E
 €y = бy –ν (бx + бz) + Δ α T
E
 €z = бz –ν (бx + бy) + Δ α T
E
} Total strains at each
point
 Relations in terms of strains:
 бx = λe + 2μ €x – (3λ+2μ) *αT
 бy = λe + 2μ €y – (3λ+2μ) *αT
 бz = λe + 2μ €z – (3λ+2μ) *αT
 ‫ح‬xy = μγxy ; ‫ح‬yz = μγyz ; ‫ح‬zx = μγzx
 Equations of equilibrium:
Where
ν = possions ratio
λ = lames constant
μ = G= modulus of rigidity
General results
 When the temperature distribution is known, the problem
of thermoelsticity is used to determining 15 functions :
 6 stress components
 6 strain components
 3 displacement components
 So as to satisfy 15 equations :
 3 equilibrium equations
 6 stress- strain relations
 6 strain – displacement relations
 Displacement boundary conditions (linear distribution):
 T(x, y, z, t) = a(t) + b(t)x + c(t)y d(t)z
“
”
€б Δ α ν λ μ

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thermalstressandstrains-150329133511-conversion-gate01 (1).pdf

  • 1. THERMALSTRESS & STRAINS By DEEPAK ROTTI Roll No: 017 KLS’s G.I.T BELGAUM
  • 2.  Temperature changes occur:  High speed travelling objects, parts & vehicles.  Heat engines and rocket engines.  Boilers, furnace etc.  Effect of temperature change :  Mechanical expansion & significance  Changes in material properties.  Expansion due to heat: Analogy:  Strains induced internally.  Hence stress induced .
  • 3. Thermal stress effects: Block of material subjected to an increase in temperature B’ Changes in temperature produce expansion or contraction of materials and result in thermal strains and thermal stresses Thermal strain εT is proportional to the temperature change ΔT :  εT = α (ΔT) (Where α is coefficient of thermal expansion)  Sign convention for thermal strains : Expansion is positive and contraction is negative
  • 4. Relation between stress (Ϭ) and change in temperature (ϪT). • Suppose we have a bar subjected to an axial load.  ε = σ / E • Also, we have an identical bar subjected to a temperature change ΔT.  εT = α (ΔT) • Equating the above two strains we will get:  σ = E α (ΔT) Increase in length of a prismatic bar due to a uniform increase in temperature 1 2 3
  • 5. Thermo-elastic stress & strain relations: Fig:A Fig:B Uniform rise in temperature (unconstrained) Hence uniform change in dimension. Non-uniform change in temperature and hence uneven stress development T=T(t, x, y, z)
  • 6. Total strain = normal strain (αT) + strain due to stress components  €x = бx –ν (бy + бz) + Δ α T E  €y = бy –ν (бx + бz) + Δ α T E  €z = бz –ν (бx + бy) + Δ α T E } Total strains at each point
  • 7.  Relations in terms of strains:  бx = λe + 2μ €x – (3λ+2μ) *αT  бy = λe + 2μ €y – (3λ+2μ) *αT  бz = λe + 2μ €z – (3λ+2μ) *αT  ‫ح‬xy = μγxy ; ‫ح‬yz = μγyz ; ‫ح‬zx = μγzx  Equations of equilibrium: Where ν = possions ratio λ = lames constant μ = G= modulus of rigidity
  • 8. General results  When the temperature distribution is known, the problem of thermoelsticity is used to determining 15 functions :  6 stress components  6 strain components  3 displacement components  So as to satisfy 15 equations :  3 equilibrium equations  6 stress- strain relations  6 strain – displacement relations  Displacement boundary conditions (linear distribution):  T(x, y, z, t) = a(t) + b(t)x + c(t)y d(t)z
  • 10. €б Δ α ν λ μ