Configuration Layout - Wing/Tail Layout and Loft-2 Online Exam Quiz
Configuration Layout - Wing/Tail Layout and Loft-2 GK Quiz. Question and Answers related to Configuration Layout - Wing/Tail Layout and Loft-2. MCQ (Multiple Choice Questions with answers about Configuration Layout - Wing/Tail Layout and Loft-2
As a designer, our job is to design a wing which has root chord Cr as 1m. What should be the approximate radius of fillet?
Options
A : 0.1m
B : 1m
C : 2m
D : 2.1m
At maximum thickness point, fillet is in __
Options
A : purely vertical plane
B : purely in hp
C : plane at an angle of less than 20? always
D : plane at 45? always
Determine the corrections or otherwise of the following assertion [A] and reason [R]:^ Assertion [A]: To generate new airfoil, we use spanwise line instead of chord line in flat wrap interpolation technique.^ Reason[R]: Chordwise line will generate flat structure from curves having different values of tangent angle.
Options
A : Both [A] and [R] are true and [R] is the correct reason for [A]
B : Both [A] and [R] are true but [R] is not the correct reason for [A]
C : Both [A] and [R] are false
D : [A] is true but [R] is false
Fillet radius is typically more at rear of the aircraft.
Options
A : TRUE
B : FALSE
C : -
D : -
For high aspect ratio strength of the wing tip vortex is low.
Options
A : TRUE
B : FALSE
C : -
D : -
If aspect ratio of wing is 8 and S=0.1m2 then, what will be the span of wing?
Options
A : 0.89m
B : 0.89cm
C : 0.89
D : 0.89inch
Wing planform is always elliptic.
Options
A : TRUE
B : FALSE
C : -
D : -
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