A tie rod made of quenched and tempered 4340 steel is used as a critical linkage in an industrial apparatus. The rod is subjected to an alternating cyclic tensile/compressive stress from 550 MPa to -550 MPa. An inspection of the rod revealed a 3.5 mm deep edge crack on the surface of the rod. Please answer the following question for the rod given the properties in the table and curve below and fracture toughness of 55 MPa√m. (NOTE: Y=1.12 for edge crack and use “a” not “2a” for the length of the crack) 1. What is the minimum crack size that would cause instantaneous fast fracture at the current maximum axial tensile loading, assuming plane strain conditions apply? If the resolution limit of the flaw detection apparatus were 1.5 mm, would this flaw be subject to detection? Show calculations to back up your conclusions.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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A tie rod made of quenched and tempered 4340 steel is used as a critical linkage in an industrial apparatus. The rod is subjected to an alternating cyclic tensile/compressive stress from 550 MPa to -550 MPa. An inspection of the rod revealed a 3.5 mm deep edge crack on the surface of the rod. Please answer the following question for the rod given the properties in the table and curve below and fracture toughness of 55 MPa√m. (NOTE: Y=1.12 for edge crack and use “a” not “2a” for the length of the crack) 

1. What is the minimum crack size that would cause instantaneous fast fracture at the current maximum axial tensile loading, assuming plane strain conditions apply? If the resolution limit of the flaw detection apparatus were 1.5 mm, would this flaw be subject to detection? Show calculations to back up your conclusions. 

### Material Properties Table

| **Property**                  | **Value**       |
|-------------------------------|-----------------|
| Modulus, E                    | 200             |
| Yield strength, \( \sigma_{y} \) (MPa) | 900             |
| Tensile strength, TS (MPa)    | 1300            |
| Elongation (%)                | 20              |
| Fracture toughness, \( K_{Ic} \) \( \left(\text{MPa} \sqrt{\text{m}}\right) \) | 55              |

### Graph Explanation

The graph on the right represents a plot of the maximum stress (\( S \)) versus the number of cycles to failure (\( N \)) for various materials. It is a S-N curve, commonly used to show the fatigue life of materials under cyclic loading.

**Key Features:**

- **X-Axis (Logarithmic scale):** Represents the cycles to failure (\( N \)), ranging from \(10^4\) to \(10^9\).
- **Y-Axis:** Represents the maximum stress (\( S \)) in MPa, ranging from 0 to 700.

**Materials Included:**

1. **Ti-5Al-2.5Sn titanium alloy**: Highest maximum stress, showing significant fatigue resistance.
2. **4340 steel**: High strength and moderately good fatigue performance.
3. **1045 steel**: Moderate fatigue performance.
4. **Ductile cast iron**: Shown with a shorter curve indicating lower cycles to failure at similar stress levels.
5. **70Cu-30Zn brass**: Lower maximum stress with moderate fatigue resistance.
6. **2014-T6 Al alloy**: Shows similar behavior to 70Cu-30Zn brass.
7. **EQ21A-T6 Mg alloy**: Displays the lowest maximum stress and fatigue life.

Each curve provides insight into how long a material can withstand cyclic stresses before failure, aiding in the selection process for engineering applications.
Transcribed Image Text:### Material Properties Table | **Property** | **Value** | |-------------------------------|-----------------| | Modulus, E | 200 | | Yield strength, \( \sigma_{y} \) (MPa) | 900 | | Tensile strength, TS (MPa) | 1300 | | Elongation (%) | 20 | | Fracture toughness, \( K_{Ic} \) \( \left(\text{MPa} \sqrt{\text{m}}\right) \) | 55 | ### Graph Explanation The graph on the right represents a plot of the maximum stress (\( S \)) versus the number of cycles to failure (\( N \)) for various materials. It is a S-N curve, commonly used to show the fatigue life of materials under cyclic loading. **Key Features:** - **X-Axis (Logarithmic scale):** Represents the cycles to failure (\( N \)), ranging from \(10^4\) to \(10^9\). - **Y-Axis:** Represents the maximum stress (\( S \)) in MPa, ranging from 0 to 700. **Materials Included:** 1. **Ti-5Al-2.5Sn titanium alloy**: Highest maximum stress, showing significant fatigue resistance. 2. **4340 steel**: High strength and moderately good fatigue performance. 3. **1045 steel**: Moderate fatigue performance. 4. **Ductile cast iron**: Shown with a shorter curve indicating lower cycles to failure at similar stress levels. 5. **70Cu-30Zn brass**: Lower maximum stress with moderate fatigue resistance. 6. **2014-T6 Al alloy**: Shows similar behavior to 70Cu-30Zn brass. 7. **EQ21A-T6 Mg alloy**: Displays the lowest maximum stress and fatigue life. Each curve provides insight into how long a material can withstand cyclic stresses before failure, aiding in the selection process for engineering applications.
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