A couple of 25 kN/m is acting at one end of a simply supported beam. ...
Consider the diagram
M = 25000 N/m, E = 250 x 109 Pa, I = 0.001 m4
Maximum deflection acts at l/√3 and is given by
= 6.42 x 10-6 m
A couple of 25 kN/m is acting at one end of a simply supported beam. ...
Problem Statement
A simply supported beam of length 1 m is subjected to a concentrated load of 25 kN/m at one end. The goal is to find the maximum deflection of the beam.
Given Data
- Load (w) = 25 kN/m = 25,000 N/m
- Length of the beam (L) = 1 m = 1000 mm
- Modulus of Elasticity (E) = 250 GPa = 250,000 MPa
- Moment of Inertia (I) = 1,000,000 mm^4
Deflection Formula
For a simply supported beam under a uniform load, the maximum deflection (δ) can be calculated using the formula:
- δ = (5wL^4) / (384EI)
Substituting Values
1. Convert the units where necessary:
- E = 250,000 MPa = 250 x 10^3 N/mm^2
- I = 1,000,000 mm^4
2. Substitute the values into the formula:
- δ = (5 * 25,000 N/m * (1000 mm)^4) / (384 * 250 x 10^3 N/mm^2 * 1,000,000 mm^4)
3. Calculate:
- δ = (5 * 25,000 * 1,000^4) / (384 * 250,000 * 1,000,000)
Final Calculation
After performing the calculation, you will find that:
- Maximum deflection δ ≈ 6.42 x 10^-6 m
Conclusion
The maximum deflection of the beam is approximately 6.42 x 10^-6 m. This result indicates that under the given loading conditions, the beam will deflect significantly, and understanding this deflection is crucial for structural design and safety assessments.
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