frm 01:26:56 a I) SE = So 8 EN J sso so AiR RI pi mason, RG, Bl van, TN BE . Ee \ Bl. sso Bea TIRANA son 3 Ne EE ". Fatigue Test Daa Fanque Failure Cele EX fom n 3 100s . I 15530 pe \ 3 or 2000 a - worm, . TNR | es - AR ~ Es x BR - 4 Be ® Actata WR § pe ETE A - PP RERROCS Fo ———
Question:
frm 01:26:56 a
I) SE =
So 8 EN
J sso so AiR RI pi
mason, RG,
Bl van, TN
BE . Ee \
Bl. sso Bea
TIRANA
son 3 Ne
EE
". Fatigue Test Daa Fanque Failure Cele EX
fom n
3 100s .
I 15530 pe \
3 or 2000 a
- worm, . TNR
| es - AR
~ Es x BR
- 4 Be
® Actata WR
§ pe
ETE A
- PP RERROCS Fo ———
This is AI generated Response.
Asked by: anil
Created at: 2025-08-19 12:51:17
Asked by: anil
Created at: 2025-08-19 12:51:17
Final Answer:
Rendered
Raw Text
Did you like this answer?
Let's break down and solve the problem step by step using the information from your image.
---
## **Problem Statement:**
A simply supported 50 mm bar is subjected to variable stresses during a duty cycle:
1. \(-200 < \sigma < 500 \text{ MPa}\) for **2000 cycles**
2. \(-100 < \sigma < 100 \text{ MPa}\) for **1000 cycles**
**Bar Properties:**
- Ultimate strength, \(S_u = 650 \text{ MPa}\)
- Yield strength, \(S_y = 600 \text{ MPa}\)
**Fatigue Test Data:**
| Fatigue Test Data (\(\sigma_a\)) | Fatigue Failure Cycle (Nf) |
| -------------------------------- | -------------------------- |
| 50 MPa | 10,000 |
| 100 MPa | 5,000 |
| 150 MPa | 4,000 |
| 250 MPa | 3,000 |
| 400 MPa | 2,500 |
| 500 MPa | 2,000 |
---
## **Steps to Solve:**
### **1. Identify Stress Ranges & Cycles:**
#### **Case 1:** \(-200 < \sigma < 500 \text{ MPa}\) for 2000 cycles
- Mean stress (\(\sigma_m\)): \(\frac{500 + (-200)}{2} = 150 \text{ MPa}\)
- Stress amplitude (\(\sigma_a\)): \(\frac{500 - (-200)}{2} = 350 \text{ MPa}\)
#### **Case 2:** \(-100 < \sigma < 100 \text{ MPa}\) for 1000 cycles
- Mean stress (\(\sigma_m\)): \(\frac{100 + (-100)}{2} = 0 \text{ MPa}\)
- Stress amplitude (\(\sigma_a\)): \(\frac{100 - (-100)}{2} = 100 \text{ MPa}\)
---
### **2. Find Fatigue Life for Each Case:**
From the table, interpolate or use values for cycles to failure at the respective amplitude.
- For **350 MPa**, interpolate between 250 MPa (3000 cycles) and 400 MPa (2500 cycles):
\[
\text{Nf at 350 MPa} = 3000 + \frac{2500 - 3000}{400 - 250} \times (350 - 250)
\]
\[
= 3000 + \frac{-500}{150} \times 100
\]
\[
= 3000 - 333.3 = 2666.7 \text{ cycles (approx.)}
\]
- For **100 MPa**, Nf = 5000 cycles.
---
### **3. Apply Miner's Rule (Linear Damage Rule):**
\[
\text{Total Damage} = \sum \frac{n_i}{N_{fi}}
\]
Where \(n_i\) = number of cycles at stress amplitude \(i\), \(N_{fi}\) = cycles to failure at that amplitude.
\[
D = \frac{2000}{2667} + \frac{1000}{5000}
\]
\[
= 0.75 + 0.2 = 0.95
\]
---
### **4. Find Number of Duty Cycles to Failure:**
Let \(n\) be the number of duty cycles.
Each duty cycle = 2000 cycles at 350 MPa + 1000 cycles at 100 MPa.
\[
D_{\text{total}} = n \left(\frac{2000}{2667} + \frac{1000}{5000}\right)
\]
Set \(D_{\text{total}} = 1\):
\[
n \times 0.95 = 1 \implies n = \frac{1}{0.95} \approx 1.05
\]
---
## **Final Answer:**
**The bar will just fail after approximately 1 duty cycle.**
If you need to consider the Goodman criterion (for mean stress), let me know and I can provide the adjustment.
---
**Let me know if you'd like to see the Goodman correction or have any other questions!**
📢 Instructions:
- Ask anything relatd to above question only.
- For new Question goto :
VIPSolutions