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

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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

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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

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Fillet radius is typically more at rear of the aircraft.

Options

A : TRUE

B : FALSE

C : -

D : -

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For high aspect ratio strength of the wing tip vortex is low.

Options

A : TRUE

B : FALSE

C : -

D : -

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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

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Wing planform is always elliptic.

Options

A : TRUE

B : FALSE

C : -

D : -

View Answer

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