Determine the internal moments at each support of the beam shown. E is constant.

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Understand the Problem

The question is asking to determine the internal moments at the supports of a beam under a specific loading condition. We will need to analyze the beam and apply principles of static equilibrium and material mechanics to find the internal moments at supports A and C.

Answer

Moment at A: $0 \, \text{N} \cdot \text{m}$; Moment at C: $-73500 \, \text{N} \cdot \text{m}$
Answer for screen readers
  • Moment at support A: $0 , \text{N} \cdot \text{m}$
  • Moment at support C: $-73500 , \text{N} \cdot \text{m}$

Steps to Solve

  1. Identify the Loads and Supports

The beam has a uniformly distributed load of $6000 , \text{N/m}$ and is supported at points A and C. We will analyze the forces acting on the system.

  1. Calculate Total Load

The total load on the beam can be found using the formula: $$ P = w \times L $$ where $w = 6000 , \text{N/m}$ and ( L = 7 , \text{m} ) (total span from A to C).

Calculating: $$ P = 6000 , \text{N/m} \times 7 , \text{m} = 42000 , \text{N} $$

  1. Determine Reaction Forces at Supports

Using static equilibrium (sum of vertical forces = 0): Let ( R_A ) be the reaction force at A and ( R_C ) at C.

The total load downward must equal the total upward forces: $$ R_A + R_C = P $$ Thus, $$ R_A + R_C = 42000 , \text{N} \tag{1} $$

To find moments, take moments around support A: $$ \sum M_A = 0 $$ The moment due to the total load: $$ 6000 \times 7 - R_C \times 7 = 0 $$ Solving for ( R_C ): $$ 42000 - 7R_C = 0 $$ $$ R_C = \frac{42000}{7} = 6000 , \text{N} $$

  1. Calculate Reaction at A

Using equation (1): $$ R_A + 6000 = 42000 $$ Solving for ( R_A ): $$ R_A = 42000 - 6000 = 36000 , \text{N} $$

  1. Determine Internal Moments at Supports

Using the calculated reactions:

  • The internal moment at support A is zero since it’s a pinned support.
  • The internal moment at support C can be calculated by taking the moment about A or C due to the loads.

Using the reaction force at C: The internal moment at C due to external load can be calculated as: For distributed load, overall moment: $$ M_C = -\frac{1}{2} \times P \times d $$ Where ( d ) is the distance to center of load from C: $$ d = \frac{L}{2} = 3.5 , \text{m} $$ Thus, $$ M_C = -\frac{1}{2} \times 42000 \times 3.5 = -73500 , \text{N} \cdot \text{m} $$

  • Moment at support A: $0 , \text{N} \cdot \text{m}$
  • Moment at support C: $-73500 , \text{N} \cdot \text{m}$

More Information

The internal moments represent the tendency of the beam to twist due to the applied load. Support A, being a pinned support, does not resist moment, while support C experiences a negative moment representing a counter-clockwise rotation.

Tips

  • Confusing the direction of moment signs. Positive moments typically cause clockwise rotation while negative causes counter-clockwise.
  • Not accounting for the total length of the beam when calculating loads and moments.

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