When a structural member is under load, predicting its
ability to withstand that load is not possible merely from the reaction force
in the member. It depends upon the internal force, cross sectional area of
the element and its material properties. Thus, a quantity that gives the
ratio of the internal force to the cross sectional area will define the
ability of the material in with standing the loads in a better way. That
quantity, i.e., the intensity of force distributed over the given area or
simply the force per unit area is called the stress.
σ= P/A ..........................................1.1
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In SI units,
force is expressed in newtons (N) and area in square meters. Consequently,
the stress has units of newtons per square meter (N/m2) or Pascals (Pa). In above figure , the
stresses are acting normal to the section XX that is perpendicular to the
axis of the bar. These stresses are called normal stresses. The stress
defined in equation 1.1 is obtained by dividing the force by the cross
sectional area and hence it represents the average value of the stress over
the entire cross section.
Consider a small area ∆A on the cross section with the
force acting on it ∆F as shown in above figure . Let the area contain a point C.
Now, the stress at the point C can be defined as,
σ = lim ∆F/∆A .............................1.2
A-->0
The average stress values obtained using equation 1.1 and
the stress value at a point from equation 1.2 may not be the same for all
cross sections and for all loading conditions.
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