A simply supported beam carrying a concentrated load W at mid -span de...
The deflection of a simply supported beam carrying a concentrated load W at mid-span can be calculated using the following formula:
δ = (W * L^3) / (48 * E * I)
where δ is the deflection, W is the load, L is the span length, E is the modulus of elasticity, and I is the moment of inertia of the beam.
Assuming a rectangular beam with width b, height h, and span length L, the moment of inertia can be calculated as:
I = (b * h^3) / 12
Substituting this in the deflection formula, we get:
δ = (W * L^3) / (48 * E * (b * h^3 / 12))
Simplifying this equation, we get:
δ = (W * L^3) / (48 * E * b * h^3)
Therefore, the deflection of a simply supported beam carrying a concentrated load W at mid-span depends on the load, span length, modulus of elasticity, width, and height of the beam.
A simply supported beam carrying a concentrated load W at mid -span de...
The ratio of their deflectin is 8/5 so it is equal to 1.6 then root two equal to 1.41:1
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