# Structures: An Airbus A340-600 with a fuselage diameter of 5.64 m is cruising at an altitude of 3...

## Question

An Airbus A340-600 with a fuselage diameter of 5.64 m is cruising at an altitude of 3000 meters. Gust applies a load that can be represented by a single load of 1500 N acting on the vertical tail at a distance of 6.5 m from the fuselage centre.

Assume an average fuselage skin thickness of t = 2 mm and a torsion moment acting on the fuselage of 8000 Nm. What is the shear stress in the fuselage skin (MT = 2qA)?

## AnswerChoose the correct answer.Choose all that apply. Correct Partially correct Incorrect Don't Know

1. A
8000 Nm
2. B
$0.04N/{\mathrm{mm}}^{2}$
3. C
160 N/m
4. D
$80000N/{m}^{2}$
5. E
$0.16N/{\mathrm{mm}}^{2}$
6. F
40 N/m
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