In a simply supported beam, maximum shear stress in a triangular cross-section (altitude h) occurs at a distance:
h/6 from neutral axis
When a beam is subjected to a transverse shear force, internal shear stresses are developed across its cross-section. These shear stresses are not uniformly distributed but vary along the depth of the beam's cross-section. The distribution of shear stress depends on the shape of the beam's cross-section. The maximum shear stress is a critical parameter in the design and analysis of beams, especially simply supported beams, to ensure they can safely carry the applied loads without failing due to shear.
For a beam with a triangular cross-section of altitude 'h', the distribution of shear stress is unique. The formula for shear stress ($\tau$) at any level 'y' from the neutral axis is given by:
$$ \tau = \frac{VQ}{Ib} $$
Where:
For a triangular cross-section with its base at the bottom and apex at the top (as is typically assumed unless stated otherwise for a simply supported beam), the key locations are:
For a triangular cross-section with its base at the bottom and its apex pointing upwards (as is commonly encountered), the maximum shear stress occurs at a specific location along its altitude 'h'.
The location of maximum shear stress in such a triangular cross-section is at a distance of \(\frac{h}{2}\) from the apex (top point) of the triangle.
Now, let's determine the distance of this point from the neutral axis:
Therefore, the maximum shear stress in a simply supported beam with a triangular cross-section (altitude h) occurs at a distance of \(\frac{h}{6}\) from the neutral axis.
Let's evaluate the given options based on our understanding of shear stress in a triangular cross-section:
Based on the analysis, the maximum shear stress for a triangular cross-section (altitude h) occurs at a distance of \(\frac{h}{6}\) from the neutral axis.
The maximum shear stress in a circular beam is
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The maximum bending stress in a curved beam having symmetrical section always occurs at the
The stresses caused by the bending moment is called -