Chegg owsora mysoline 0 Noticatons 8+ fen a . a ones Bas Tad Th oc Th Be Ty vant Sa B18 Ms 20 3p G18 MDs. oy 050 3d o Rap 7 n i! Ge CEO® Pee = Qs cuEoOoOE ABOBO@ Neem, Ne
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Chegg owsora mysoline 0 Noticatons 8+
fen a .
a ones Bas Tad Th oc Th Be Ty vant Sa B18 Ms 20 3p G18 MDs. oy 050 3d
o Rap
7 n i!
Ge CEO®
Pee = Qs cuEoOoOE ABOBO@ Neem, Ne
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Asked by: kasireddi sai
Created at: 2025-10-18 17:22:36
Asked by: kasireddi sai
Created at: 2025-10-18 17:22:36
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# Analysis of Shaft Design Problem
## Problem Overview
The task is to **determine the critical diameter of a shaft** (using the DE-Goodman criteria and a design factor of 1.5) based on loading conditions and to find the factor of safety against yielding.
### Provided Data
- **Ultimate strength, $S_{ut}$:** 848 MPa
- **Yield strength, $S_y$:** 618 MPa
- **Shaft diameter at critical location:** **50 mm**
- **Fillet radius:** .50 mm
- **Design factor:** 1.5
## Steps for Solution
### 1. **Identify Critical Section**
- The critical section is usually where the maximum moment or torque occurs, or where stress concentration is highest (e.g., at keyseats or fillets).
### 2. **Calculate Stresses**
- **Bending Stress:**
\[
\sigma_b = \frac{M \cdot c}{I}
\]
- **Torsional Shear Stress:**
\[
\tau_t = \frac{T \cdot c}{J}
\]
- Where:
- \( M \) = Bending moment
- \( T \) = Torque
- \( c \) = Outer radius = 25 mm = .025 m
- \( I \) (moment of inertia for a solid shaft) = \( \frac{\pi d^4}{64} \)
- \( J \) (polar moment of inertia for a solid shaft) = \( \frac{\pi d^4}{32} \)
### 3. **Find Combined Stress**
Using the maximum shear stress theory (or DE-Goodman for fatigue if fluctuating loads are present):
\[
\sigma_{eq} = \sqrt{\sigma_b^2 + 3\tau_t^2}
\]
### 4. **Apply Factor of Safety**
\[
\text{Allowable stress} = \frac{S_y}{n}
\]
Where \( n = 1.5 \).
### 5. **Calculate Factor of Safety Against Yielding**
\[
n_{actual} = \frac{S_y}{\sigma_{eq}}
\]
---
## Sample Calculation (Based on Provided Diameter)
### **Step 1: Calculate Allowable Stress**
\[
\text{Allowable Stress} = \frac{618\ \text{MPa}}{1.5} = 412\ \text{MPa}
\]
### **Step 2: Factor of Safety Against Yielding**
Assuming you calculated an equivalent stress at the critical section (let's denote it as \( \sigma_{eq} \)):
\[
n_{actual} = \frac{618\ \text{MPa}}{\sigma_{eq}}
\]
---
## **Summary Table**
| Parameter | Value | Unit |
|---------------------------------|--------------|---------|
| Shaft diameter (critical) | 50 | mm |
| Allowable stress (with n=1.5) | 412 | MPa |
| Yield strength, \(S_y\) | 618 | MPa |
| Ultimate strength, \(S_{ut}\) | 848 | MPa |
| Fillet radius | .50 | mm |
| Factor of safety (against yield)| (Plug your calculated \(\sigma_{eq}\)) | |
---
## **To Complete the Solution**
- Plug in the actual values for the bending moment and torque at the critical section (from the diagram and loading).
- Calculate combined stress.
- Compute the factor of safety against yielding as shown above.
---
**Note:** If you provide the actual values for \( M \) and \( T \), I can help you with exact calculations. If you need further help with DE-Goodman fatigue safety factor, please specify if the loading is fluctuating.
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