Deriving Moment & Elastic Curve Equations for Incomplete Triangular Load on Beam

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To derive the moment and elastic curve equations for an incomplete triangular load on a beam with a pin at one end and a roller at L/2, it is essential to define the load as a distributed load that starts at zero and increases linearly to the roller. The deflection equations can be expressed as Δ = Δ(x) for x ≤ L/2 and Δ = θ2*(x-L/2) for x > L/2. Understanding the relationship between the load distribution and the resulting deflection is crucial for accurate calculations. The extension method is necessary for deriving these equations, particularly in determining the moment at various points along the beam. Accurate derivation of these equations is vital for structural analysis and design.
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I was wondering how you would derive the moment and elastic curve equations for an incomplete triangular load. Say you have a pin at the left end of the beam and a roller at L/2 from the left, and a triangular load that goes from the pin and ends at the roller. I know you have to do some kind of extension, but how do you come up with the formula.
 
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When you say "triangular load", you mean a distributed load that's zero at the left end and increases linearly to the roller at L/2?
 
If you know Δ(x) and θ2 for a simply supported beam as a function of L' = L/2 with a triangular load then the deflection would be:

Δ = Δ(x) for x=<L/2
= θ2*(x-L/2) for x>=L/2
 
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@timthereaper yes
 
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