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Cantilever beam - Couple moment Mo at free end Calculator













Formula

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

Cantilever Beam - Couple Moment \( M_o \) at Free End


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 the free end, it induces a pure bending effect without generating shear force. This loading condition primarily influences the bending moment distribution and deflection of the beam.

Key Concepts

  • Couple Moment \( M_o \): A moment (torque) applied at the free end, measured in units of force × distance (e.g., N·m or lb·ft).
  • Fixed End: The end rigidly attached to a support, resisting both rotation and translation.
  • Free End: The unsupported end where the moment is applied, causing rotational displacement.
  • Shear Force: Zero throughout the beam since the applied couple moment does not generate a resultant force.
  • Bending Moment: The moment remains constant throughout the beam, equal to \( M_o \).
  • Deflection: The beam experiences angular rotation at the free end without transverse displacement.

Behavior of the Cantilever Beam


  1. Reaction Forces:
    • At the fixed end, the beam generates a reaction moment \( M_R = M_o \) to balance the applied couple moment.
    • No vertical reaction force is produced.
  2. Shear Force Diagram: The shear force remains zero throughout the entire length of the beam.
  3. Bending Moment Diagram:
    • The bending moment is constant along the beam and equal to \( M_o \).
    • Unlike other loading conditions, there is no variation in the moment distribution.
  4. Deflection: The beam undergoes rotation at the free end, calculated using: \[ \theta_{\text{max}} = \frac{M_o L}{EI} \] where \( E \) is the modulus of elasticity, \( I \) is the moment of inertia, and \( L \) is the beam length.

Applications


  • Structural Engineering: Used in beams and supports subjected to pure moments at their free ends.
  • Mechanical Systems: Common in robotic arms, torque shafts, and rotating cantilevered components.
  • Construction: Helps analyze the effects of end moments in overhanging structures.

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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