Question: Fuselage bending loads are carried by ___
Options
A : keelson
B : tail
C : nelson
D : ribs
Configuration Layout - Structural Considerations more questions
A spar is located at 65% of MAC from leading....
A typical large airliner has outer diameter of 20in. find....
A wing has chord of 1m. Find the appropriate range....
If possible, we should avoid using any structural cutout.
Longerons are used to oppose __
To decrease the weight of a typical commercial fuselage, stringers....
To reduce weight of the structural member we can __
Aerodynamic Coefficients more Online Exam Quiz
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