Question 1
What is the key geometric assumption behind a thin-walled idealisation?
Question 2
In a thin-walled idealisation, the wall is usually represented by what?
Question 3
Why is a thin-walled idealisation used in aerospace structures?
Question 4
Which item is a typical thin-walled aerospace component?
Question 5
What is usually assumed about stress across the wall thickness in a thin-walled section?
