Step 1: Understanding the Question and Frame Determinacy: The portal frame has a hinged support (2 reaction components) and a roller support (1 reaction component). Total reactions \(R=3\). The equations of static equilibrium are 3 (\(\Sigma F_x=0, \Sigma F_y=0, \Sigma M=0\)). Since \(R=3\), the frame is statically determinate. We can find the reactions using these equations. Let the hinge be A (left) and the roller be D (right). The top joints are B (left) and C (right).
Step 2: Calculate Support Reactions: We apply the equations of static equilibrium to the entire frame.
- \(\Sigma F_x = 0\): Let \(A_x\) be the horizontal reaction at A.
\[ 50 - A_x = 0 \implies A_x = 50 \text{ kN (acting towards the left)} \] - \(\Sigma M_A = 0\): Taking moments about the hinge support A (clockwise positive).
\[ (50 \text{ kN} \times 3 \text{ m}) + (90 \text{ kN} \times 2 \text{ m}) - (D_y \times 4 \text{ m}) = 0 \] \[ 150 + 180 - 4D_y = 0 \] \[ 4D_y = 330 \implies D_y = 82.5 \text{ kN (upwards)} \] - \(\Sigma F_y = 0\): Let \(A_y\) be the vertical reaction at A.
\[ A_y + D_y - 90 = 0 \] \[ A_y + 82.5 - 90 = 0 \implies A_y = 7.5 \text{ kN (upwards)} \]
Step 3: Bending Moment Calculation: Now, we calculate the bending moments at critical points (joints and under loads).
- Support A (Hinge): \(M_A = 0\)
- Support D (Roller): \(M_D = 0\)
- Joint B (top of column AB): The bending moment at B is caused by the horizontal reaction \(A_x\). \[ M_{B} = -A_x \times (\text{height}) = -50 \text{ kN} \times 3 \text{ m} = -150 \text{ kNm} \] (The negative sign indicates a hogging moment, causing tension on the left side of the column).
- Joint C (top of column CD): Since there is no horizontal reaction at D, the shear force in column CD is zero. Therefore, the bending moment along column CD is zero. Thus, \(M_C = 0\).
- Midspan of beam BC (point E): The shear force just to the right of B is \(A_y = 7.5\) kN. The moment at E can be found by considering the beam segment BE. \[ M_E = M_B + (\text{Area of SFD from B to E}) = -150 \text{ kNm} + (7.5 \text{ kN} \times 2 \text{ m}) \] \[ M_E = -150 + 15 = -135 \text{ kNm} \]
Step 4: Determine Maximum Absolute Bending Moment: The bending moments at the critical points are:
- \(M_A = 0\) kNm
- \(M_B = -150\) kNm
- \(M_E = -135\) kNm
- \(M_C = 0\) kNm
- \(M_D = 0\) kNm
Comparing the absolute values: \(|0|, |0|, |-150|, |-135|, |0|\). The maximum absolute value is 150 kNm.