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What is Bending Stress

A Technical Overview

Bending Stresses in Engineering: Concepts, Examples, and Applications

Introduction to Bending Stresses

Bending stresses are critical considerations in engineering, particularly in the design of beams, shafts, and other structural components subjected to transverse loads. When a structural member is bent, stresses develop due to the material's resistance to deformation. This article explores bending stresses, their theoretical basis, derivations, and applications, along with practical examples.


Definition of Bending Stress

Bending stress is the internal stress induced in a material when an external bending moment is applied. It is typically categorized as either tensile stress or compressive stress depending on the location within the cross-section of the member.

The bending stress at any point in the cross-section is given by:


σ = (M · y) / I


  • σ: Bending stress (Pa or N/m²)
  • M: Bending moment (N·m)
  • y: Distance from the neutral axis (m)
  • I: Moment of inertia of the cross-section about the neutral axis (m⁴)

This equation assumes:

  • The material is homogeneous and isotropic.
  • The beam experiences pure bending (no shear force).
  • The deflections are small.



Key Concepts in Bending Stresses

  1. Neutral Axis (NA): The line within the cross-section where the bending stress is zero.
  2. Moment of Inertia (I): A geometric property that quantifies a cross-section's resistance to bending.
  3. Maximum Bending Stress: The maximum stress occurs at the farthest distance (ymax) from the neutral axis:

    σmax = (M · ymax) / I

  4. Beam Theory: Derived from Euler-Bernoulli beam theory, which assumes that plane sections remain plane and perpendicular to the beam's axis after bending.


Worked Examples


Worked Example 1: Calculating Bending Stress in a Beam

Problem: A simply supported beam with a span of 6 m carries a uniformly distributed load of 20 kN/m over its entire length. The beam has a rectangular cross-section with a width of 300 mm and a height of 500 mm. Calculate the maximum bending stress in the beam.


Solution:


Calculate the maximum bending moment:

Mmax = (w · ) / 8


Substitute: w = 20 kN/m = 20 × 10³ N/m, L = 6 m


Mmax = (20 × 10³ · 6²) / 8 = 90 kN·m = 90 × 10³ N·m


Calculate the moment of inertia:

I = (b · ) / 12


Substitute: b = 0.3 m, h = 0.5 m

I = (0.3 · 0.5³) / 12 = 3.125 × 10-3 m⁴


Calculate the maximum bending stress:

ymax = h / 2 = 0.5 / 2 = 0.25 m


σmax = (Mmax · ymax) / I


Substitute: σmax(90 × 10³ · 0.25) / (3.125 × 10-3) = 7.2 MPa


Answer: The maximum bending stress in the beam is 7.2 MPa.


Example 2: Designing a Beam

Problem: Design a simply supported beam to carry a central point load of 50 kN over a span of 4 m. The beam has a rectangular cross-section with a width-to-height ratio of 1:2. The allowable bending stress is 8 MPa. Determine the dimensions of the beam.


Solution:


Calculate the maximum bending moment:

Mmax = (P · L) / 4


Substitute: P = 50 × 10³ N, L = 4 m

Mmax = (50 × 10³ · 4) / 4 = 50 × 10³ N·m


Relate maximum stress to dimensions:

σmax = (6 · Mmax) / (b · )


Substitute: σmax = 8 × 10⁶ Pa, Mmax = 50 × 10³ N·m

b · = (6 · 50 × 10³) / (8 × 10⁶) = 0.0375 m³


Relate width and height:

h = 2b, substitute into the volume equation:

b · (2b)² = 0.0375


b = 0.21 m, h = 0.42 m


Answer: The beam should have dimensions b = 0.21 m and h = 0.42 m.


Applications of Bending Stresses in Engineering

  • Structural Design: Used in beams, bridges, and buildings to ensure structural integrity.
  • Machine Components: Design of shafts, levers, and gears subjected to bending loads.
  • Material Testing: Understanding material behavior under bending to establish yield and failure criteria.
  • Aerospace and Automotive: Analysis of wings, chassis, and frames for safety and performance.


Further Reading: Beam Bending - An Overview


References

  1. Beer, F. P., Johnston, E. R., & DeWolf, J. T. (2011). Mechanics of Materials. McGraw-Hill Education.
  2. Gere, J. M., & Goodno, B. J. (2012). Mechanics of Materials. Cengage Learning.
  3. Hibbeler, R. C. (2017). Mechanics of Materials. Pearson Education.
  4. Timoshenko, S. P., & Gere, J. M. (1961). Theory of Elastic Stability. McGraw-Hill.
  5. Megson, T. H. G. (2019). Aircraft Structures for Engineering Students. Butterworth-Heinemann.


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