The stress intensity factor for a partial-through thickness crack is given by where a is the length of of crack through a wall thickness t. If the crack is 10 mm deep in a wall 20 mm thick determine whether the wall will support a stress of 190 MPa if it is made from steel with fracture toughness of 30 MPA m1/2
The stress intensity factor for a partial-through thickness crack is given by where a is the length of of crack through a wall thickness t. If the crack is 10 mm deep in a wall 20 mm thick determine whether the wall will support a stress of 190 MPa if it is made from steel with fracture toughness of 30 MPA m1/2
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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The stress intensity factor for a partial-through thickness crack is given by
where a is the length of of crack through a wall thickness t. If the crack is 10 mm
deep in a wall 20 mm thick determine whether the wall will support a stress of 190
MPa if it is made from steel with fracture toughness of 30 MPA m1/2
![**Q5. The stress intensity factor for a partial-through thickness crack is given by**
\[ K = \sigma \sqrt{\pi a} \sqrt{\sec \frac{\pi a}{3t}} \]
- **Explanation:**
- \( K \) is the stress intensity factor.
- \( \sigma \) represents the applied stress.
- \( a \) is the crack length.
- \( t \) is the thickness of the material.
- The expression involves a square root and a trigonometric secant function, indicating that the stress intensity factor depends on geometric and material properties.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F08a0d1a7-4387-4b00-bd8e-a511cc6565f1%2Fb7702ea5-eccc-4490-851d-438a6ec43876%2Fobx5n7m_processed.png&w=3840&q=75)
Transcribed Image Text:**Q5. The stress intensity factor for a partial-through thickness crack is given by**
\[ K = \sigma \sqrt{\pi a} \sqrt{\sec \frac{\pi a}{3t}} \]
- **Explanation:**
- \( K \) is the stress intensity factor.
- \( \sigma \) represents the applied stress.
- \( a \) is the crack length.
- \( t \) is the thickness of the material.
- The expression involves a square root and a trigonometric secant function, indicating that the stress intensity factor depends on geometric and material properties.
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