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

In summary, the equations for the moment and elastic curve for an incomplete triangular load on a simply supported beam with a pin at the left end, a roller at L/2 from the left, and a distributed load that increases linearly from the pin to the roller can be derived by using the formulas for deflection and angle of rotation for a simply supported beam with a triangular load. The deflection is equal to the deflection at x for x less than or equal to L/2 and the angle of rotation multiplied by x minus L/2 for x greater than L/2.
  • #1
Quantumsatire
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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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  • #2
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?
 
  • #3
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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  • #4
@timthereaper yes
 
  • #5


To derive the moment and elastic curve equations for an incomplete triangular load on a beam, we can use the principles of statics and mechanics of materials. The first step would be to draw a free body diagram of the beam, including all external forces and reactions. In this case, we have a pin support at the left end, a roller support at L/2 from the left, and a triangular load acting on the beam between these two supports.

Next, we can apply the equations of static equilibrium to determine the reactions at the supports. For a pin support, we know that it can only exert a vertical reaction force, while a roller support can exert both vertical and horizontal reaction forces. By summing the forces in the vertical and horizontal directions, we can solve for the reactions at the supports.

Once we have the reactions, we can use the principle of superposition to determine the internal forces and moments at any point along the beam. This means that we can break down the triangular load into smaller, simpler loads, such as point loads or distributed loads, and analyze each one separately. Then, we can sum the individual results to get the overall response of the beam.

To determine the moment equation, we can use the moment equation M = Fd, where M is the moment, F is the force, and d is the perpendicular distance from the point of interest to the line of action of the force. By applying this equation to each individual load, we can determine the moment at any point along the beam.

To determine the elastic curve equation, we can use the equation EIy'' = M, where E is the modulus of elasticity, I is the moment of inertia, y'' is the second derivative of the deflection curve, and M is the moment. By integrating this equation twice and applying boundary conditions, we can solve for the deflection of the beam at any point.

In summary, to derive the moment and elastic curve equations for an incomplete triangular load on a beam, we need to apply the principles of statics and mechanics of materials, use the equations of equilibrium and superposition, and solve for the reactions and internal forces using appropriate equations.
 

What is beam deflection loading?

Beam deflection loading is the deformation of a beam under the influence of external forces, such as bending or twisting. It is an important concept in structural engineering and is used to determine the strength and stability of a beam.

What factors affect beam deflection?

The factors that affect beam deflection include the type and magnitude of the applied load, the material and shape of the beam, and the support conditions. In general, stiffer and stronger materials will have less deflection, while longer and thinner beams will have more deflection.

How is beam deflection calculated?

Beam deflection can be calculated using mathematical equations, such as the Euler-Bernoulli beam theory or the Timoshenko beam theory. These equations take into account the various factors that affect beam deflection and provide a quantitative value for the amount of deflection at a given point on the beam.

Why is beam deflection important?

Beam deflection is important because it directly affects the strength and stability of a structure. Excessive deflection can cause a structure to fail, while minimal deflection can indicate that the structure is able to safely support the applied loads.

What are some common methods for reducing beam deflection?

Some common methods for reducing beam deflection include increasing the stiffness and strength of the beam through material selection or cross-sectional shape, adding supports or braces along the beam, and redistributing the load to multiple beams. Additionally, adjusting the spacing of supports can also help reduce deflection.

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