Configuration Layout - Structural Considerations Online Exam Quiz
Configuration Layout - Structural Considerations GK Quiz. Question and Answers related to Configuration Layout - Structural Considerations. MCQ (Multiple Choice Questions with answers about Configuration Layout - Structural Considerations
__ is key parameter for vulnerability.
Options
A : Vulnerable area
B : RCS
C : IR
D : Visual area
A spar is located at 65% of MAC from leading edge. If spar is positioned in such way that distance between t.e. and spar is 2m then, estimate chord of wing.
Options
A : 5.71m
B : 6.8
C : 4.4
D : 6.5
A typical large airliner has outer diameter of 20in. find the approximate value of diameter for passenger compartment.
Options
A : 12in
B : 34in
C : 20in
D : 24in
A wing has chord of 1m. Find the appropriate range of the front spar position from l.e.
Options
A : 0.2m-0.3m
B : 0.9m-1.5m
C : 3.2
D : 1.2
FMEA stands for?
Options
A : Failure modes and effect analysis
B : Failure mass and effect analysis
C : Failure mass and effective analogy
D : Failure modes and effect analogy
FMEA will consider ___
Options
A : which battle damage can affect individual aircraft components?
B : lift
C : weight by an aircraft
D : rcs
Fuselage bending loads are carried by ___
Options
A : keelson
B : tail
C : nelson
D : ribs
If possible, we should avoid using any structural cutout.
Options
A : TRUE
B : FALSE
C : -
D : -
Longerons are used to oppose __
Options
A : bending
B : expansion only
C : contraction only
D : drag
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
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