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Question

A triangular beam section having base width ‘b’ and height ‘d’ the section modulus for beam strength is

The correct answer is \(\rm \frac{bd^2}{24}\)

Calculating Section Modulus for a Triangular Beam Section

The question asks for the section modulus of a triangular beam section with base width 'b' and height 'd'. The section modulus is a geometric property of a cross-section that is used in the design of beams or flexural members. It relates the maximum stress in a beam to the bending moment.

The section modulus (\(Z\)) is defined as the ratio of the moment of inertia (\(I\)) about the neutral axis to the distance of the extreme fiber (\(y_{max}\)) from the neutral axis.

\(Z = \frac{I}{y_{max}}\)

For a triangular section with base 'b' and height 'd', the neutral axis for bending is located at the centroid of the triangle. The centroid is located at a distance of \(d/3\) from the base and \(2d/3\) from the apex (the top vertex opposite the base).

The moment of inertia of a triangular section about its centroidal axis (which is the neutral axis for bending) parallel to the base is given by:

\(I = \frac{bd^3}{36}\)

The extreme fibers are the points farthest from the neutral axis. For a triangle, these are the base and the apex.

  • Distance from the neutral axis to the base: \(y_{base} = \frac{d}{3}\)
  • Distance from the neutral axis to the apex: \(y_{apex} = \frac{2d}{3}\)

The maximum distance to the extreme fiber from the neutral axis is the larger of these two values:

\(y_{max} = \max\left(\frac{d}{3}, \frac{2d}{3}\right) = \frac{2d}{3}\)

Now we can calculate the section modulus (\(Z\)) using the formula \(Z = \frac{I}{y_{max}}\):

\(Z = \frac{\frac{bd^3}{36}}{\frac{2d}{3}}\)

To simplify the expression, we can multiply by the reciprocal of the denominator:

\(Z = \frac{bd^3}{36} \times \frac{3}{2d}\)

\(Z = \frac{b \times d^3 \times 3}{36 \times 2 \times d}\)

\(Z = \frac{3bd^3}{72d}\)

Cancel out common terms (\(3\) from numerator and \(36/12\) from denominator, and \(d\) from numerator and denominator):

\(Z = \frac{bd^{3-1}}{72/3}\)

\(Z = \frac{bd^2}{24}\)

Thus, the section modulus for a triangular beam section with base 'b' and height 'd' is \(\frac{bd^2}{24}\).

Revision Table: Triangular Section Properties

Understanding the key properties of a triangular section is crucial for structural analysis.

  • Area: \(\frac{1}{2}bd\)
  • Centroid Location (from base): \(\frac{d}{3}\)
  • Centroid Location (from apex): \(\frac{2d}{3}\)
  • Moment of Inertia (\(I\)) about centroidal axis (parallel to base): \(\frac{bd^3}{36}\)
  • Section Modulus (\(Z\)) for bending about centroidal axis: \(\frac{bd^2}{24}\)

Additional Information on Section Modulus

The section modulus is a direct measure of the strength of a beam in bending. A larger section modulus indicates a greater resistance to bending stress. The maximum bending stress (\(\sigma_{max}\)) in a beam is related to the bending moment (\(M\)) and the section modulus (\(Z\)) by the formula:

\(\sigma_{max} = \frac{M}{Z}\)

This formula shows that for a given bending moment, a larger section modulus will result in a smaller maximum bending stress, making the beam stronger in bending. The shape and size of the cross-section significantly influence its section modulus. Efficient shapes for resisting bending, like I-beams or hollow sections, maximize the moment of inertia while keeping the material away from the neutral axis, thus increasing the section modulus.

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Important Questions from Plastic Analysis

  1. The shape factor for a solid circular section of diameter D is equal to:

  2. In a steel beam, when the width to thickness ratio of the compression flange is sufficiently large, local buckling of compression flange may occur even before extreme fibre yields. Such sections are generally known as

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  4. The plastic theory is generally used for

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