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
- Reaction Forces:
- At the fixed end, the beam generates a reaction moment \( M_R = M_o \).
- No vertical reaction force is produced.
- Shear Force Diagram: The shear force is zero throughout the beam.
- 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.
- 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 |