- •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
4.9 Statically indeterminate systems
Statically
indeterminate systems can be solved from conditions of equal or zero
displacement of chosen points.
If both parts of the structure
have the same length, the fraction of the external load accepted by
each part of the structure is proportional to its rigidity - the
product of modulus of elasticity by cross-sectional area.
Stress
is proportional to the corresponding fraction of external load. At
the same time the stress is inversely proportional to the
cross-sectional area.
This means that absolute values of the
stresses in both parts are equal.
For
an angle of 60 degrees, length of cable 1 is twice as long as cable
2.
Displacement d2
is twice as large as d1.
The fraction of external force depends on rigidity, cable
length and the displacement.
Cables 1 and 3 accept only 20% of
the external vertical load.
The
shaft parts have different torsional stiffness and a common part in
the center. The common part is rotated at the same angle for both
parts, the angle of twist. Absolute values of the angle of twist for
the left and right parts are equal.
The
gap d1
can be deleted by elastic deformation of the cables. The equilibrium
equation for moments relative to point O shows that forces in the
cables are inversely proportional to the distance from point
O.
Both
beams have equal deflection that is proportional to L3.
Cutting the length in half increases the fraction of external force
by 23=8.
Shapes
of the the moment diagram are similar, but for the second beam there
are reaction moments in embedded ends. They shift the curve down and
decrease the maximum moment. The second beam is more rigid.
The
bending moment is at a maximum in the support zones. The maximum
value of the bending moment M=FL over the right support does not
depend on the number of supports.
To
solve the system it is necessary to find the shown unknown inner
forces and reactions from conditions of equal displacements. There
are no transverse forces for symmetrical system. Number of equations
n depends on chosen equivalent scheme. The smaller the number the
better.
4.10 Three-dimensional structures
For
three-dimensional structures there are six components of moments and
forces in a point. If we cut the curved beam perpendicular to the
beam axis the torque is equal to the product of Force by Arm : F*r1
and the bending moment is equal to F*r2.
Internal forces are equal to the sum of corresponding projections of
external forces.
The
figure shows examples of bending moment and torque diagrams for
three-dimensional structures. The diagrams are built by the
above-mentioned rules.
There
are tensile as well as compressive stresses at external surface of
the arc. The bending moment changes its sign.
For
a thin-walled sphere, absolute value of radial stress at the external
surface is equal to external pressure. It is smaller than meridian
and tangential stress components.
The
first step of the analysis includes determination of reactions in the
supports. There is symmetry in the structure. There are no torque or
bending moments in part of the structure.
The conclusion is
purely theoretical, the structure is not stable. Loss of stability
causes additional forces and moments for all parts of the
structure.
