1. Shearing Stress Distribution in Rectangular cross Section
Let us consider the rectangular section ABCD of a beam as shown in figure.
We have assumed one layer EF at a distance y from the neutral axis of the beam section.
The shear force acting on section is = F
b= Width of the rectangular section
d= Depth of the rectangular section
N.A: Neutral axis of the beam section
EF: Layer of the beam at a distance y from the neutral axis of the beam section
A- Area of section CDEF, where shear stress is to be determined
A = b (d/2 - y)
ȳ = Distance of C.G of the area CDEF from neutral axis of the beam section
ȳ = y + (d/2 - y)/2 = (d/2 +y)/2
I = Moment of inertia of the given section about the neutral axis (mm4)
I = bd3/12
Shear stress at a section will be given by following formula substitute the values in the above shear stress equation, the shear stress in the layer EF is,when y= d/2 , the shear stress is zero
y = 0 , the shear stress at neutral axis is maximum and equal to τmax
τmax = 3/2 F/bd
The average shear stress
τave = F/bd =Shear force / Area of cross section
For a rectangular section,
The maximum shear stress τmax = 1.5 τave
2. Shearing Stress Distribution in Triangular cross Section
Let us consider a triangular section of base b and height h. Its centroid is located at a distance h/3 from the base.
The shear force acting on section is = F.
Assume b′ & h′ be the width & height of the triangle above the plane EF.From same triangles,
b / b′= h/ h′
b′ = bh′ / h
h′ = ((2/3) h - y )
b′ = (b/ h) ( (2/3) h - y )
Centroid of the triangle above the plane EF, through the neutral axis y' = ( y +( h′ /3 ))
On putting the value of h′
y' = y + (1/3)((2/3)h - y ) =(2/3)(y+(h/3))
Moment of this triangular area around the neutral axis Q = Ay'The shear stress T, at the plane EF is
For shear stress τ to be maximum, dT / dy = 0 ,
(h /3) - 2 y = 0
∴ y = h/6
The maximum shear stress is at a distance form the base of the triangle is = h/3 +y
= h/ 3+ h/6 = h/2
∴ Maximum shear stress is at a distance of h/2 form the base of the triangle, that is also at a distance of h/6 from the centroidal axis.
Putting y = h/ 6 in the equation for the shear stress, the maximum shear stress
The shear stress at the neutral axis, (when y = 0),
τNA = (F /3I ) (2h.h/9)
= (8/3) ×(F/bh)
The shear stress distribution diagram is as shown in Figure.
Note:
The average shear stress = τave = F/A = 2F/bh
The maximum shear stress in Triangular section
τmax = 3Vx/bh = 1.5 τave
The shear stress at N.A in Triangular section
τNA = 8Vx/3bh = 4/3 τave
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