How Can You Solve the Simply Supported Beam Equations?

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  • Thread starter Ackbach
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In summary, the simply supported beam equations are mathematical formulas used to analyze and design beams that are supported on both ends and have no other external forces acting on them. The formula for calculating the deflection of a simply supported beam is D = (5 * w * L^4) / (384 * E * I), and the maximum bending moment can be determined by analyzing the forces and loads acting on the beam. Assumptions are made in these equations, such as a straight and uniform beam, and the equations can be solved using various methods such as hand calculations, numerical methods, or computer software.
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Ackbach
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Here is this week's POTW:

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Solve the simply supported beam equations:
\begin{align*}
u_{tt}&=-u_{xxxx}, \qquad 0<x<1, \qquad 0<t<\infty \\
u(0,t)&=0 \\
u_{xx}(0,t)&=0 \\
u(1,t)&=0 \\
u_{xx}(1,t)&=0 \\
u(x,0)&=f(x) \\
u_{t}(x,0)&=g(x)
\end{align*}

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  • #2
No one solved this week's POTW, which is stolen lock, stock, and barrel from Farlow's Partial Differential Equations for Scientists and Engineers. His solution follows:

We use the separation of variables method and look for arbitrary periodic solutions; that is, vibrations of the form
$$(21.3) \qquad\qquad\qquad u(x,t)=X(x)[A \sin(\omega t)+B \cos(\omega t)].$$
Note that by choosing the solution in the form (21.3), we are essentially saying that the separation constant in the separation-of-variables method has been chosen to be negative.

We now substitute equation (21.3) into the beam equation to get the ODE in $X(x)$.
$$X^{iv}-\omega^2 X=0,$$
which has the general solution
$$X(x)=C \cos\left(\sqrt{\omega} \, x\right)+D \sin\left(\sqrt{\omega} \, x\right)+E \cosh\left(\sqrt{\omega} \, x\right)+F \sinh\left(\sqrt{\omega} \, x\right).$$
To find the constants $C, D, E,$ and $F,$ we substitute this expression into the BCs, giving
\begin{align*}
u(0,t)&=0 \implies X(0) T(t)=0 \implies X(0)=0 \implies C+E=0 \\
u_{xx}(0,t)&=0 \implies X''(0) T(t)=0 \implies X''(0)=0 \implies -C+E=0,
\end{align*}
which together imply that $C=E=0$.
\begin{align*}
u(1,t)&=0\implies D\sin\left(\sqrt{\omega}\right)+F\sinh\left(\sqrt{\omega}\right)=0 \\
u_{xx}(1,t)&=0\implies -D\sin\left(\sqrt{\omega}\right)+F\sinh\left(\sqrt{\omega}\right)=0.
\end{align*}
From these last two equations, we arrive at the expressions
\begin{align*}
F\sinh\left(\sqrt{\omega}\right)&=0 \\
D \sin\left(\sqrt{\omega}\right)&=0
\end{align*}
from which we can conclude
\begin{align*}
F&=0 \\
\sin\left(\sqrt{\omega}\right)&=0 \implies \omega=(n\pi)^2,\quad n=1,2,\dots
\end{align*}
In other words, the natural frequencies of the simply supported beam are
$$\omega_n=(n\pi)^2$$
and the fundamental solutions $u_n$ (solutions of the PDE and BCs) are
$$u_n(x,t)=X_n(x) T_n(t)=\left(a_n \sin\left[(n\pi)^2 t\right]+b_n \cos\left[(n\pi)^2t\right] \right) \sin(n\pi x).$$
Now, since the PDE and BCs are linear and homogeneous, we can conclude that the sum
$$(21.4) \qquad\qquad\qquad\boxed{u(x,t)=\sum_{n=1}^{\infty}\left(a_n \sin\left[(n\pi)^2 t\right]+b_n \cos\left[(n\pi)^2t\right] \right) \sin(n\pi x)} $$
also satisfies the PDE and BCs. Hence, all that remains to do is choose the constants $a_n$ and $b_n$ in such a way that the ICs are satisfied. Substituting equation (21.4) into the ICs gives us
\begin{align*}
u(x,0)&=f(x)=\sum_{n=1}^{\infty}b_n \sin(n\pi x) \\
u_t(x,0)&=g(x)=\sum_{n=1}^{\infty}(n\pi)^2 a_n \sin(n\pi x),
\end{align*}
and using the fact that the family $\{\sin(n\pi x)\}$ is orthogonal on the interval $[0,1]$ gives us
\begin{align*}
a_n&=\frac{2}{(n\pi)^2} \int_0^1 g(x) \, \sin(n\pi x) \, dx \\
b_n&=2\int_0^1 f(x) \, \sin(n\pi x) \, dx.
\end{align*}
Hence, the solution is given by (21.4), and $a_n$ and $b_n$ are given by the last two equations.
 

What are the simply supported beam equations?

The simply supported beam equations are mathematical equations that describe the behavior and deflection of a beam that is supported on both ends and has no other external forces acting on it. These equations are used to analyze and design structures such as bridges and buildings.

What is the formula for calculating the deflection of a simply supported beam?

The formula for calculating the deflection of a simply supported beam is:
D = (5 * w * L^4) / (384 * E * I)
where D is the deflection, w is the load applied to the beam, L is the length of the beam, E is the elastic modulus of the material, and I is the moment of inertia of the beam's cross-sectional area.

How do you determine the maximum bending moment of a simply supported beam?

The maximum bending moment of a simply supported beam can be determined by analyzing the forces and loads acting on the beam using the equations of static equilibrium. The maximum bending moment occurs at the center of the beam and is equal to the product of the load and the distance from the support to the center of the beam.

What are the assumptions made in the simply supported beam equations?

The assumptions made in the simply supported beam equations include:
- The beam is straight and uniform
- The beam is loaded in the center
- The beam is supported on both ends
- The material is elastic and obeys Hooke's law
- The beam is subjected to static loading
These assumptions may not hold true in all cases and therefore, the results obtained from the equations should be used with caution.

How can you solve the simply supported beam equations?

The simply supported beam equations can be solved using various methods such as:
- Hand calculations using the formulas
- Numerical methods such as finite element analysis
- Computer software and programs
The method chosen will depend on the complexity of the problem and the accuracy required for the results.

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