- •Главная
- •1.1 Напряжений и концентраторы
- •1.1.3 Концентраторы напряжения
- •1.3 Stress concentration factor
- •1.7 Elastic-plastic stress concentration
- •1.8 Joints: bolts and welds
- •3. Механические свойства конструкционных материалов
- •3.1 Напряженности испытания
- •3.2 Stress - strain diagram
- •3.3 Testing schemes
- •3.4 Strength
- •4 Прочность материалов
- •4.1 Tension and compression
- •4.2 Shear and torsion
- •4.3 Stress-strain state
- •4.4 Bending: force and moment diagrams
- •4.5 Geometrical characteristics of sections
- •4.6 Bending: stress and deformation
- •4.7 Mixed mode loading
- •4.8 Buckling
- •4.9 Statically indeterminate systems
- •4.10 Three-dimensional structures
- •References
- •5. Theory of elasticity
- •5.1 Deformation
- •5.2 Stress
- •5.3 Hooke's law
- •5.4 Plane problems
- •5.5 Torsion
- •5.6 Bending
- •5.7 Polar coordinates
- •5.8 Plates
- •5.9 Shells
- •5.10 Contact stresses
- •6.2 Distribution functions
- •6.3 Structural models of reliability
- •6.4 Limiting state
- •6.5 Dispersion
- •6.6 Durabilty
- •6.7 Design by reliability criterion
- •6.8 Risk
- •6.9 Safety classes
- •6.10 Risk : structural and social
- •References
- •7 Materials science
- •7.1 Crystalline solids
- •7.2 Mechanical properties
- •7.3 Failure
- •7.4 Phase diagrams
- •7.5 Heat treatment of metals and alloys
- •7.6 Corrosion of metals and alloys
- •7.7 Casting
- •7.8 Polymers
- •7.9 Composites
- •7.10 Forming of metals
- •8.2 Mechanical properties
- •8.3 Stress concentration
- •8.4 Defects
- •8.5 Residual Stress
- •8.6 Strength
- •8.7 Fatigue strength
- •8.8 Fracture
- •8.9 Weldability
- •References
- •9 Composites
- •9.1 Structure of composites
- •9.2 Fibers
- •9.3 Rigidity
- •9.4 Strength
- •9.5 Crack resistance
- •9.6 Optimization
- •9.7 Fatigue and temperature effect
- •9.8 Reliability
- •9.9 Joints
- •9.10 Material selection
- •References
- •10 Finite element analysis
- •10.1 Finite element method
- •10.2 Finite elements
- •10.3 Meshing
- •10.4 Boundary conditions
- •10.5 Deformation
- •10.6 Accuracy
- •10.7 Heat transfer analysis
- •10.8 Dynamics
- •10.9 Computational fluid dynamics
- •10.10 Design analysis
- •References
10.7 Heat transfer analysis
Steady-State
or Transient Heat Transfer Analysis is devoted to predicting the
temperature distribution for an object exposed to heating, radiation,
convection and conduction. Thermal Stress Analysis predicts stresses,
displacements due to thermal expansion or contraction.
To
perform heat transfer analysis or static structural analysis the same
types of elements can be used. There is no need to decrease the order
of elements or to remesh the model. For three-dimensional (3D) brick
elements there are 3 nodal displacements for static analysis. Nodal
temperature is an additional variable. Therefore, there are 4
variables per node for the thermal stress analysis. The structural
stiffness matrix does not depend on boundary conditions or nodal
temperature.
Temperature
change causes thermal expansion or contraction. High temperature
causes thermal expansion of a solid. Uniform heating results in
deformation only, not thermal stress. High gradient of temperature
causes distortion of the beam. Thermal stresses are caused by
temperature gradient. The smaller the distance between nodes with
different temperatures, the larger the distortion and thermal
stresses.
Cooling
causes contraction and tensile stress sz
in most of the elements. The stress does not depend on the width of
the plate. The stress at the left-hand side of the notched specimen
is very small. There is a stress gradient in the net-section A - B.
The stress is the largest in element A.
Oil
quenching of a steel structure can be modeled by transient heat
transfer module. The results are transferred to static analysis to
calculate the thermal stresses. Quenching causes contraction of
external surfaces. The contraction causes the tensile stress on those
surfaces. The intersection of thin and thick walls causes the highest
thermal stresses.
A
pressure vessel with bimetal steel walls was heated till 400oC.
The coefficient of thermal expansion is larger for stainless steel.
The stainless steel layer tries to expand but the titanium alloy
layer does not have such a large deformation. There is a negative
tangential thermal stress in the stainless steel. There is additional
compressive thermal stress in the stainless steel near the layer's
intersection.
Uniform
heating of the rigid ring will expand it mostly in the tangential
direction. There is a smaller displacement in the radial direction.
Thin walled dome-shape plate will have a larger radial displacement.
It causes the central points to move upwards.
A
cold drop of water on a hot metal surface causes thermal cracking due
to local tensile stress. The temperature distribution in the
structure is used as the loading condition for a structural analysis
to calculate thermal stress.
The temperature can be
calculated using the differential equation governing transient heat
transfer with a heat source. In this case:
k is the heat
transfer coefficient;
T is temperature;
t is time;
Q(t)
is the heat source.
