Express the internal shear and moment in terms of x and then draw the shear and moment diagrams. You must use the 'BRUTE FORCE' method of sections, drawing your section FBDs for ea... Express the internal shear and moment in terms of x and then draw the shear and moment diagrams. You must use the 'BRUTE FORCE' method of sections, drawing your section FBDs for each region, and coming up with an exact formula for V(x) and M(x) in each region.

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Understand the Problem

The question is asking to express the internal shear (V(x)) and moment (M(x)) for a given beam in terms of x, using the method of sections. It requires drawing Free Body Diagrams (FBDs) for each section and deriving exact formulas for the shear and moment in each region.

Answer

Shear: $V(x) = \frac{w_0 L}{2} - w_0 x$ (for $0 < x < L/2$), $V(x) = w_0\left(\frac{L}{2} - x\right)$ (for $L/2 < x < L$). Moment: $M(x) = \frac{w_0 L}{2}x - \frac{w_0 x^2}{2}$ (for $0 < x < L/2$); $M(x) = -\left(w_0\left(\frac{L}{2} - x\right)(L - x)\right)$ (for $L/2 < x < L$).
Answer for screen readers

The shear and moment equations for each region are:

  • For $0 < x < \frac{L}{2}$:

    • Shear: $V(x) = \frac{w_0 L}{2} - w_0 x$
    • Moment: $M(x) = \frac{w_0 L}{2} \cdot x - \frac{w_0 x^2}{2}$
  • For $\frac{L}{2} < x < L$:

    • Shear: $V(x) = w_0 (L - x) - \frac{w_0 L}{2} = w_0(L/2 - x)$
    • Moment: $M(x) = -\left(-\frac{w_0 L}{2} + w_0 (L - x)\right)(L - x)$

Steps to Solve

  1. Determine Reaction Forces

First, find the support reactions at points A and B. For a uniformly distributed load $w_0$ over the beam of length $L$, the total load is $W = w_0 \cdot L$.

Using static equilibrium:

  • The sum of vertical forces: $R_A + R_B - W = 0$
  • The sum of moments about point A: $\sum M_A = 0 \Rightarrow R_B \cdot L - W \cdot \frac{L}{2} = 0$

From the moment equation, we can solve for $R_B$: $$ R_B = \frac{W \cdot \frac{L}{2}}{L} = \frac{w_0 L}{2} $$

Now substituting $R_B$ back to find $R_A$: $$ R_A = W - R_B = w_0 L - \frac{w_0 L}{2} = \frac{w_0 L}{2} $$

  1. Divide the Beam into Sections

Next, divide the beam into two sections to analyze separately:

  • Section 1: from A to a point $x$ where $0 < x < L/2$
  • Section 2: from $x$ to B where $L/2 < x < L$
  1. Shear Force for Section 1 (A to x)

For Section 1:

  • The internal shear force $V(x)$ can be determined by taking moments about point A.

Using equilibrium: $$ \sum F_y = 0: R_A - w_0 x - V(x) = 0 $$

Which gives: $$ V(x) = R_A - w_0 x = \frac{w_0 L}{2} - w_0 x $$

  1. Bending Moment for Section 1 (A to x)

The internal moment $M(x)$ can be found from: $$ M(x) = R_A \cdot x - \frac{w_0 x^2}{2} $$

Substituting $R_A$: $$ M(x) = \frac{w_0 L}{2} \cdot x - \frac{w_0 x^2}{2} $$

  1. Shear Force for Section 2 (x to B)

For Section 2: Assume the distance from A to B is $L$. The internal shear force $V(x)$ is given by: $$ \sum F_y = 0: V(x) + R_B - w_0 \cdot \left(L - x\right) = 0 $$

Substituting for $R_B$: $$ V(x) = -\frac{w_0 L}{2} + w_0 \cdot (L - x) $$

  1. Bending Moment for Section 2 (x to B)

For the bending moment: $$ M(x) = M_{B} - V(x) \cdot (L - x) $$

Since the moment at point B is 0 (simply supported), we have: $$ M(x) = 0 - \left(-\frac{w_0 L}{2} + w_0 (L - x)\right)(L - x) $$

Calculating this will give the moment in terms of $x$.

The shear and moment equations for each region are:

  • For $0 < x < \frac{L}{2}$:

    • Shear: $V(x) = \frac{w_0 L}{2} - w_0 x$
    • Moment: $M(x) = \frac{w_0 L}{2} \cdot x - \frac{w_0 x^2}{2}$
  • For $\frac{L}{2} < x < L$:

    • Shear: $V(x) = w_0 (L - x) - \frac{w_0 L}{2} = w_0(L/2 - x)$
    • Moment: $M(x) = -\left(-\frac{w_0 L}{2} + w_0 (L - x)\right)(L - x)$

More Information

The equations provided express how shear and moment change along the beam from supports A to B. This method uses equilibrium principles to derive the internal forces and moments in structural analysis.

Tips

  • Forgetting to include the reactions at the supports while calculating shear and moment.
  • Misapplying the equations in different sections according to the location of the cut.
  • Not maintaining consistent signs for shear and moment calculations based on loading direction.

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