# A fuselage with a perfect circular cross-section with a diameter of 3.6 m and a skin thickness of 1.2 mm assume a pressure?

Differential While flying at cruising altitude of 45 kpa.

Calculate the circumferential stress in mpa, induced by the pressure differential.

### 1 Answer

Relevance

- oil field trashLv 71 month ago
Below is an excellent article on the subject.

- Log in to reply to the answers

Still have questions? Get answers by asking now.