Question: Solve for the moment and shear diagram using the structural analysis of Hibbler given loads: $10$ kN point load, $5$ kN/m and $8$ kN/m distributed loads, and spans $5$ m, $8$ m, $2$ m, $3$ m, $2$ m.
1. **Problem Statement:**
We have a structural frame/beam with a $10$ kN point load, distributed loads of $5$ kN/m and $8$ kN/m, and spans of $5$ m, $8$ m, $2$ m, $3$ m, and $2$ m. We need to find the shear force and bending moment diagrams using Hibbler's structural analysis method.
2. **Step 1: Calculate Reactions at Supports**
- Use equilibrium equations: $$\sum F_x=0, \sum F_y=0, \sum M=0$$
- Calculate equivalent point loads for distributed loads:
- For $5$ kN/m over $5$ m: $$5 \times 5 = 25\text{ kN}$$ acting at midpoint $2.5$ m from left.
- For $8$ kN/m over $8$ m: $$8 \times 8 = 64\text{ kN}$$ acting at midpoint $4$ m from left of that span.
3. **Step 2: Apply Equilibrium Equations**
- Sum vertical forces:
$$R_A + R_B = 10 + 25 + 64$$
$$R_A + R_B = 99\text{ kN}$$
- Sum moments about left support $A$:
$$\sum M_A = 0 = -10 \times 0 + 25 \times 2.5 + 64 \times (5 + 4) - R_B \times (5 + 8)$$
$$0 = 0 + 62.5 + 576 - R_B \times 13$$
$$R_B = \frac{638.5}{13} = 49.12\text{ kN}$$
- Then,
$$R_A = 99 - 49.12 = 49.88\text{ kN}$$
4. **Step 3: Construct Shear Force Diagram (V)**
- Start from left support $A$ with $+49.88$ kN.
- Subtract point load $10$ kN at $0$ m: $$49.88 - 10 = 39.88\text{ kN}$$
- Subtract distributed load $5$ kN/m over $5$ m:
$$V = 39.88 - 5x, \quad 0 \leq x \leq 5$$
At $x=5$: $$39.88 - 5 \times 5 = 14.88\text{ kN}$$
- Jump down by $25$ kN equivalent load at midpoint.
- Subtract distributed load $8$ kN/m over $8$ m:
$$V = 14.88 - 8y, \quad 0 \leq y \leq 8$$
At $y=8$: $$14.88 - 8 \times 8 = -49.12\text{ kN}$$
- At right support $B$, shear returns to zero.
5. **Step 4: Construct Bending Moment Diagram (M)**
- Integrate shear diagram:
- From $0$ to $5$ m:
$$M(x) = 49.88x - \frac{5x^2}{2} - 10(x - 0)H(x - 0)$$
- From $5$ to $13$ m:
$$M(x) = M(5) + \int_5^x V(x) dx$$
- Calculate moments at key points:
- At $x=0$: $$M=0$$
- At $x=5$: $$M = 49.88 \times 5 - \frac{5 \times 5^2}{2} - 10 \times 5 = 249.4 - 62.5 - 50 = 136.9\text{ kNm}$$
- At $x=13$: $$M = 0$$ (support)
6. **Step 5: Summary**
- Reactions: $$R_A = 49.88\text{ kN}, R_B = 49.12\text{ kN}$$
- Shear force varies linearly under distributed loads and jumps at point loads.
- Bending moment diagram is parabolic under distributed loads and linear between loads.
This completes the shear and moment diagram calculation using Hibbler's structural analysis approach.