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Cantilever beam - Couple moment Mo at any point Calculator















Cantilever Beam - Couple Moment \( M_o \) at Any Point


A cantilever beam is a structural element fixed at one end and free at the other. When a couple moment \( M_o \) is applied at any point along the beam, it induces specific effects such as deflection, bending moment, and shear force. Unlike a concentrated load, a couple moment does not produce a resultant force but instead creates pure bending.

Key Concepts

  • Couple Moment \( M_o \): A moment (torque) applied at a specific point, consisting of two equal and opposite forces. Measured in units of force × distance (e.g., N·m or lb·ft).
  • Fixed End: The end rigidly attached to a support, resisting rotation and translation.
  • Free End: The unsupported end that experiences deflection due to the applied moment.
  • Shear Force: Zero throughout the beam because the couple moment does not create any shear force.
  • Bending Moment: Varies along the beam and changes abruptly at the point of the couple moment.
  • Deflection: The displacement of the beam, maximum at the free end.

Behavior of the Cantilever Beam


  1. Reaction Forces:
    • At the fixed end, the beam generates a reaction moment \( M_R = M_o \).
    • No vertical reaction force is produced.
  2. Shear Force Diagram: The shear force is zero throughout the beam.
  3. Bending Moment Diagram:
    • Constant between the fixed end and the point of the couple moment.
    • Changes abruptly by \( M_o \) at the point of application.
    • Remains constant beyond the point of application.
  4. Deflection: Maximum at the free end, calculated using beam deflection formulas.

Applications


  • Engineering Design: Used in structures subjected to torsional or rotational loads.
  • Mechanical Systems: Applied in shafts, levers, and supports.
  • Construction: Used to calculate the stability of cantilevered structures under rotational forces.

Formula

Parameter Formula
Deflection \(y_{AC}\) \(y_{AC} = \frac{M_0 x^2}{2EI}\)
Deflection \(y_{CB}\) \(y_{CB} = \frac{M_0 a}{2EI} (2x - a)\)
Deflection at \(x = L\) (\(y_{MAx}\) for segment AC) \(y_{MAx} = \frac{M_0 a}{2EI} (2L - a)\)
Slope \(\theta_{AC}\) \(\theta_{AC} = \frac{M_0 x}{EI}\)
Slope \(\theta_{CB}\) (\(\theta_C = \theta_B\)) \(\theta_{CB} = \theta_C = \theta_B = \frac{M_0 a}{EI}\)
Moment \(M_{AC}\) (\(M_A\)) \(M_{AC} = M_A = -M_0\)
Moment \(M_{CB}\) (\(M_B\)) \(M_{CB} = M_B = 0\)
Shear \(V_{AC}\) (\(V_A = V_C\)) \(V_{AC} = V_A = V_C = 0\)
Shear \(V_{CB}\) (\(V_C = V_B\)) \(V_{CB} = V_C = V_B = 0\)
Reactions \(R_A\) \(R_A = 0\)

Definitions

Symbol Physical quantity Units
E·I Flexural rigidity N·m², Pa·m⁴
y Deflection or deformation m
θ Slope, Angle of rotation -
x Distance from support (origin) m
L Length of beam (without overhang) m
M Moment, Bending moment, Couple moment applied N·m
P Concentrated load, Point load, Concentrated force N
w Distributed load, Load per unit length N/m
R Reaction load, reaction force N
V Shear force, shear N
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