Give step-by-step solution with explanation and final answer:The plane object ABCD distorts into the shape shown by the dotted line. Find the shear strain yxy at point
C, shear strain yxy at point D and & of side CD.
y
14 mm
5
mm HHIRRUREE
CETTE TREE J {9 mm
4 mm [i B |
c {
i
|
350 mm !
ll :
pid
E ~~ {3mm
D| A N
IVRHARY 500 mm
6 mm } P
Hits 1 i
} sh RY
BV Ei
Question:
Give step-by-step solution with explanation and final answer:The plane object ABCD distorts into the shape shown by the dotted line. Find the shear strain yxy at point
C, shear strain yxy at point D and & of side CD.
y
14 mm
5
mm HHIRRUREE
CETTE TREE J {9 mm
4 mm [i B |
c {
i
|
350 mm !
ll :
pid
E ~~ {3mm
D| A N
IVRHARY 500 mm
6 mm } P
Hits 1 i
} sh RY
BV Ei
This is AI generated Response.
Asked by: manish kumar
Created at: 2025-09-07 13:09:48
Final Answer:
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Let’s solve the problem step by step:
**Given:**
- The original rectangle \(ABCD\) is distorted as shown.
- We are to find:
1. Shear strain \(\gamma_{xy}\) at point **C**
2. Shear strain \(\gamma_{xy}\) at point **D**
3. Normal strain \(\epsilon_x\) of side **CD**
---
### **Step 1: Coordinates Before and After Deformation**
Let’s assign the original coordinates:
| Point | Original (x, y) | Deformed (x', y') |
|-------|-------------------|----------------------|
| A | (500, 0) | (500+6, 0+3) = (506, 3) |
| B | (500, 350) | (500+14, 350+9) = (514, 359) |
| C | (0, 350) | (0+4, 350+5) = (4, 355) |
| D | (0, 0) | (0, 0) |
---
### **Step 2: Strain Calculations**
#### **A. Shear Strain \(\gamma_{xy}\) at Point C**
Shear strain at a point is given by:
\[
\gamma_{xy} = \frac{\partial u}{\partial y} + \frac{\partial v}{\partial x}
\]
where \(u\) and \(v\) are the displacements in \(x\) and \(y\).
- For small strain and for a rectangle, approximate:
- \(\frac{\partial u}{\partial y}\) is the change in \(x\)-displacement per unit \(y\) (vertical edge)
- \(\frac{\partial v}{\partial x}\) is the change in \(y\)-displacement per unit \(x\) (horizontal edge)
##### **Find Displacements:**
- At C: \(u_C = 4\), \(v_C = 5\)
- At D: \(u_D = 0\), \(v_D = 0\)
- At B: \(u_B = 14\), \(v_B = 9\)
- At A: \(u_A = 6\), \(v_A = 3\)
##### **Partial Derivatives at C:**
\[
\frac{\partial u}{\partial y} \approx \frac{u_B - u_A - (u_C - u_D)}{(y_B - y_A) + (y_C - y_D)}
\]
But since C and D are on the left, use:
\[
\frac{\partial u}{\partial y} \approx \frac{u_C - u_D}{y_C - y_D} = \frac{4 - 0}{350 - 0} = \frac{4}{350} = 0.01143
\]
\[
\frac{\partial v}{\partial x} \approx \frac{v_A - v_D}{x_A - x_D} = \frac{3 - 0}{500 - 0} = \frac{3}{500} = 0.006
\]
\[
\gamma_{xy, C} = 0.01143 + 0.006 = \boxed{0.01743}
\]
---
#### **B. Shear Strain \(\gamma_{xy}\) at Point D**
\[
\frac{\partial u}{\partial y} \approx \frac{u_A - u_D}{y_A - y_D} = \frac{6 - 0}{0 - 0} = \text{undefined} \ (\text{so use C-D instead})
\]
But along vertical edge, use C-D as above:
\[
\frac{\partial u}{\partial y} \approx \frac{u_C - u_D}{y_C - y_D} = \frac{4}{350} = 0.01143
\]
\[
\frac{\partial v}{\partial x} \approx \frac{v_D - v_C}{x_D - x_C} = \frac{0 - 5}{0 - 4} = \frac{-5}{-4} = 1.25
\]
But this seems odd; check along D-A:
\[
\frac{\partial v}{\partial x} \approx \frac{v_A - v_D}{x_A - x_D} = \frac{3}{500} = 0.006
\]
So at D:
\[
\gamma_{xy, D} = 0.01143 + 0.006 = \boxed{0.01743}
\]
(Same as at C, since both are on the left edge.)
---
#### **C. Normal (Axial) Strain \(\epsilon_x\) of Side CD**
\[
\epsilon_x = \frac{\Delta L}{L_0}
\]
Where \(L_0 = 500 \text{ mm}\) (original length CD), and \(\Delta L\) is increase in length after deformation.
- CD original: from \((0,0)\) to \((500,0)\)
- After deformation: from \((0,0)\) to \((4,355)\)
Find new length:
\[
L = \sqrt{(4-0)^2 + (355-0)^2} = \sqrt{4^2 + 355^2} = \sqrt{16 + 126025} = \sqrt{126041} \approx 355.16 \text{ mm}
\]
Wait, this is vertical side. For CD (horizontal):
Original: \(D(0,0)\) to \(C(0,350)\) (vertical edge, length 350 mm)
After deformation: \(D(0,0)\) to \(C(4,355)\)
\[
L = \sqrt{(4-0)^2 + (355-0)^2} = \sqrt{16 + 126025} = \sqrt{126041} \approx 355.17 \text{ mm}
\]
So,
\[
\Delta L = 355.17 - 350 = 5.17 \text{ mm}
\]
\[
\epsilon_x = \frac{5.17}{350} = 0.0148
\]
---
## **Final Answers:**
1. **Shear strain \(\gamma_{xy}\) at C:**
\(\boxed{0.01743}\)
2. **Shear strain \(\gamma_{xy}\) at D:**
\(\boxed{0.01743}\)
3. **Normal strain \(\epsilon_x\) of side CD:**
\(\boxed{0.0148}\)
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