Question: Span-loading is defined as __
Options
A : distribution of weight along span as lift distribution
B : thrust loading
C : wing loading
D : inverse of power loading
Configuration Layout - Structural Considerations more questions
Fuselage bending loads are carried by ___
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 __
Vulnerability of an aircraft is ability of the aircraft __
Vulnerable area will be same for each and every aircraft.
We can minimize the weight of the structural member by....
Aerodynamic Coefficients more Online Exam Quiz
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