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This is AI generated Response.
Asked by: Md Israrul Haque
Created at: 2025-10-26 03:21:11
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Here's a summarized and organized version of the handwritten solution for clarity:
---
# Solution Summary
## Given Data
- Cross-sectional area, \(A = 500\, \text{mm}^2\)
- Modulus of Elasticity, \(E = 200\, \text{GPa}\)
---
## Step 1: Free Body Diagram
- Coordinates and dimensions are drawn, with points \(A, B, C, D\).
- Dimensions:
- \(AB = 1.6\, \text{m}\)
- \(AD = 1.2\, \text{m}\)
- \(DC = .9\, \text{m}\)
- \(BC = 4.8\, \text{m}\)
- \(DE = 2.5\, \text{m}\)
- Vertical and horizontal components are labeled.
---
## Step 2: Equations of Equilibrium
### Horizontal (x-direction):
\[
\sum F_x = \Rightarrow A_x - D_x = \quad \Rightarrow A_x = D_x = 5\, \text{kN}
\]
### Vertical (y-direction):
\[
\sum F_y = \Rightarrow -4.8 + A_y = \Rightarrow A_y = 4.8\, \text{kN}
\]
---
## Step 3: Joint Method for Force Components
### At Point A:
- \(\tan \theta_1 = \frac{1.2}{1.6} \Rightarrow \theta_1 = 36.07^\circ\)
- Horizontal component:
\[
F_{AB} \cos 36.07^\circ = 5\, \text{kN}
\]
\[
F_{AB} = \frac{5}{\cos 36.07^\circ} \approx 6.25\, \text{kN}
\]
### At Point D:
- \(\tan \theta_2 = \frac{1.2}{1.6} \Rightarrow \theta_2 = 36.07^\circ\)
- Vertical component:
\[
F_{DB} \sin 36.07^\circ = 1.75\, \text{kN}
\]
\[
F_{DB} = \frac{1.75}{\sin 36.07^\circ} \approx 3.00\, \text{kN}
\]
---
## Step 4: Force Calculation
- \(F_{DC}\) from equilibrium:
\[
F_{DC} = -3.60\, \text{kN}
\]
- Components at C:
- \(\theta_3 = 53.13^\circ\)
- \(F_{CB} = 6.00\, \text{kN}\)
---
## Step 5: Axial Strain and Stress
- Axial deformation:
\[
\delta = \frac{F \times L}{A \times E}
\]
- Using the force \(F_{AB} = 6.25\, \text{kN}\):
\[
\text{Stress } \sigma = \frac{F}{A} \approx \frac{6.25 \times 10^3}{500 \times 10^{-6}} = 12.5\, \text{MPa}
\]
---
## Step 6: Deflection Calculations
- Using the equilibrium equations, deflections are found via the method of joints and applying trigonometric relations.
---
## Final Note:
- The diagram and forces are used to determine the internal forces in each member.
- The displacement and stress are calculated based on these forces and material properties.
---
If you need a detailed step-by-step calculation or a specific part clarified, please specify!
Question:
Do not skipped anything from the above attached image and do not add anything from this.
This is AI generated Response.
Asked by: Md Israrul Haque
Created at: 2025-10-26 03:27:09
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# Solution Summary
## Given Data
- Cross-sectional area, \( A = 500\, \text{mm}^2 \)
- Modulus of Elasticity, \( E = 200\, \text{GPa} \)
---
## Step 1: Free Body Diagram
- **Coordinates and dimensions**:
- Points: \( A, B, C, D \)
- Dimensions:
- \( AB = 1.6\, \text{m} \)
- \( AD = 1.0\, \text{m} \)
- \( DC = 0.9\, \text{m} \)
- \( BC = 4.8\, \text{m} \)
---
## Step 2: Equations of Equilibrium
### Horizontal (x-direction):
\[
\sum F_x = A_x + D_x = 0
\]
### Vertical (y-direction):
\[
\sum F_y = -4.8 + A_y + D_y = 0
\]
From which we get:
- \( A_y = 4.8\, \text{kN} \)
- \( D_y = 0\, \text{kN} \)
---
## Step 3: Joint Method for Force Components
### At Point A:
- **Angle Calculation**:
\[
\tan \theta_1 = \frac{1.0}{1.6} \Rightarrow \theta_1 = 36.87^\circ
\]
- **Horizontal Component**:
\[
F_{AB} \cos 36.87^\circ = 4.8 \quad \Rightarrow \quad F_{AB} = \frac{4.8}{\cos 36.87^\circ} \approx 6.00\, \text{kN}
\]
### At Point D:
- **Vertical Component**:
\[
F_{DB} \sin 36.87^\circ = 1.0\, \text{kN} \quad \Rightarrow \quad F_{DB} = \frac{1.0}{\sin 36.87^\circ} \approx 1.6\, \text{kN}
\]
---
## Step 4: Force Calculation
- **Equilibrium at C**:
\[
F_{DC} = -3.0\, \text{kN}
\]
---
## Step 5: Axial Strain and Stress
- **Axial Deformation**:
\[
\delta = \frac{F \times L}{A \times E}
\]
- **Stress Calculation**:
\[
\sigma = \frac{F}{A} \approx \frac{6.00 \times 10^3}{500 \times 10^{-6}} = 12.0\, \text{MPa}
\]
---
## Step 6: Deflection Calculations
- **Deflection**:
- Using equilibrium equations and trigonometric relations based on forces.
---
## Final Note
- The internal forces in each member are determined using the diagram and equilibrium conditions.
- Stress and deformation are calculated based on the forces and material properties.
If further breakdown or specifics are needed, please specify!