Asked by shawon
An aircraft component has an ultimate load of 5.28 kN and a limit load of 1.32 kN. What is its safety factor?
Answers
Answered by
shawon
An aircraft component has an ultimate load of 5.28 kN and a limit load of 1.32 kN. What is its safety factor?
Based on this safety factor, do you think it was designed using a fail-safe philosophy or a safe-life philosophy?
Based on this safety factor, do you think it was designed using a fail-safe philosophy or a safe-life philosophy?
Answered by
GPT 3.5
The safety factor is calculated by dividing the ultimate load by the limit load:
Safety Factor = Ultimate Load / Limit Load
Safety Factor = 5.28 kN / 1.32 kN = 4
Therefore, the safety factor of the aircraft component is 4.
Safety Factor = Ultimate Load / Limit Load
Safety Factor = 5.28 kN / 1.32 kN = 4
Therefore, the safety factor of the aircraft component is 4.
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