- •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
10.10 Design analysis
FEA
is used to optimize design, guarantee safety, reduce design-cycle
time, weight, costs, and the need for testing.
Practitioners
can use FEA
- to prove design safety;
- to meet code
requirements;
- to modify an existing design;
- to test
new and competing designs;
- to peer inside design and see
phenomenon that cannot be measured with experimental methods.
Now
FEA packages are integrated with solid modeling and computer aided
design (CAD) systems. CAD is the use of geometric or solid modeling
programs to aid in the creation or modification of a design. A
structure may be drawn in solid model form by one of the many CAD
packages available. Wireframe is a geometric representation of 3D
model as outlined by its outer edges. The model is transferred to a
FE software, where it is meshed and boundary conditions are
specified. The stresses, displacements, temperatures and other
parameters are results of the FE solution. The results help to make
decisions on changes in structure design, loads or service regimes.
CAD and FEA are becoming integrated.
A FEA analysis is not
simply translating a CAD file and watching the results. Considerable
care and skill has to be employed to be sure that the results
correspond to the reality and all scenarios are taken into
account.
Transferring
a model from a CAD system assumes some simplification of the model.
The fillets in the area of maximum stress concentration are the
subject of detailed analysis.
Fillets
are not always modeled in detail. If the calculated maximum stress is
large then one of the possible ways to guarantee the safety of the
new structure is in correct design of fillets which can decrease
stress concentrations.
FEA
is also used to calculate nominal stresses in different regions of
the structure. The FEA can be useful in comparing of old and new
designs with similar manufacturing technologies. If nominal stresses
in the model of a new design are smaller than for the old the
conclusion of the analysis is the new design is at least as safe as
the old one.
There
are about 100 types of standard finite elements in commercial FE
packages. Automatic meshing procedures can divide the sub-areas on
standard elements. There are no plane elements with 5 or 11 nodes.
The number of nodes in a finite element cannot be chosen arbitrary.
FEA solves problems using
Stress
Analysis
Stresses, displacements, deflections are calculated for static
loading.
Steady-state
or Transient Heat Transfer
Predicting temperature distribution for an object exposed to heating,
radiation, convection and conduction.
Thermal
Stress Analysis
Stresses and displacement due to thermal expansion are a subject of
the analysis.
Transient
Dynamic
Objects in rapid motion or under impact are studied to obtain maximum
stresses, deflection. Dynamic incremental nonlinear analysis assumes
not one, but many solution steps for nonlinear system. Time for
solution of the problem is significantly higher than for static
analysis problem.
Modal
Analysis
Vibration characteristics such as natural frequencies and mode shapes
are calculated.
Fluid
Flow
Fluid flow in gases, air, and water is modeled to find temperatures,
pressures, velocities, etc.
Linear
Buckling
Calculates the load at which a structure is likely to fail due to
elastic instability.
Non
Linear Analysis
Analysis for large deflections and nonlinear material behavior such
as plastic.
Nonlinear
problems are solved by with step-by-step increments of applied loads
F. At each step the material constant (effective modulus of
elasticity) changes depending on the level of stress intensity in the
FE for a previous step and material behavior ('stress-strain'
diagram). At each loading step the components of the stiffness matrix
change according to the new level of stress. It is better to avoid
infinitely large or negative diagonal components of the stiffness
matrix. This can lead to numerical "oscillation" and errors
in the analysis.
