Structural Mechanics Unit 1 Flashcards
what is the difference between a structural material and a structure
structure - is an arrangement of one or more materials in a way that is designed to sustained loads
structural material - any material that may be used to construct a structure
what are the symbols for stress, strain and co-efficient of viscosity
stress - σ (sigma)
strain - ε (epsilon)
co-efficient of viscosity - η (eta)
what is stress denied as, the equation and units
force per cross-sectional area
stress = force/area
units = newton per metre squared or Pascal
what would handle more force, a bar with a bigger or small cross-sectional area
bar with a bigger cross-sectional area
in regards to strain, what would the difference be in elongation of 2 bars, 1 of which is longer than the other
the longest bar would elongate more
if bar 1, is twice the length of bar 2, it will elongate twice as much
what does the stress-strain curve show
how the material deforms/behaves as it is loaded
on a stress-strain curve, what does the letters P,E,Y,H,V and R represent
P = proportional limit E = elastic limit Y = yield strength H = strain hardening V = ultimate stress R = rupture
in regards to the stress-strain curve, was is the relationship between stress and strain at very small loads
there is a linear relationship between stress and strain
i.e. if stress doubles, strain doubles
what happens at P = proportional limit
relationship between stress and strain is not proportional anymore
what happens at E = Elastic limit
before here, if the load is removed from the material, the material will recover back to its original shape and size
this is the elastic region
after the elastic limit, the material will NOT return to its original shape and size after the load is removed
what happens at Y = Yield point
after this point, the material will undergo considerable elongation without an increase in stress
- highlighted by the flatness of the region on the graph
- material is displaying perfect plastic behaviour (no elastic recovery)
what happens after the E = Elastic limit
material is in the plastic region
material deforms instantly under applied load
material may partially recover to original size and shape when load is removed, but NOT completely like in the elastic region
what are the section of the stress-strain curve in order they happen
elastic region
plastic region
strain hardening
necking
what is happening in the strain hardening region
the material is undergoing changes in its atomic and crystalline structure
results in an increased resistance to further deformation
what is U = ultimate strength point on the stress-strain curve
occurs at highest point on the graph
after this point, strain increases with a reduction in stress and ‘necking’ happens
the stress the bar can withstand decreases, NOT sue to any loss of material but due to reduction in cross-sectional area of the bar
how can the true stress-strain curve be obtained
calculate the stress at the narrowest part of the neck
what is the rupture point, R
point at which the material breaks
stress at this point is called the rupture strength
what is a material that can only handle a small amount of strain before breaking described as
brittle
what is a material that deformed plastically before breaking described as
ductile
what is the difference between ductile and brittle materials
a brittle material ruptures after a small amount of strain whilst a ductile material can deform considerably before rupturing
what is Hooke’s Law
Up to a certain level of stress (the proportional limit), the strain is proportional to the applied stress
what is the equation for Young’s modulus and the other name for it
Youngs Modulus (E) = stress/strain
Unit = N m-2 or Pa
modulus of elasticity
what does a large young modulus mean
that the material requires a large amount of stress is required to produce a small strain i.e. material is stiff
vice versa, a small young’s modulus means only a small amount of stress is needed to produce a big strain i.e. material is flexible
what is the definition of rigidity and equation
ability to resist axial deformation
rigidity = E x cross sectional area
[rigidity = EA]
Unit = Newton (N)