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Wing Geometry - Aircraft Design MCQ Questions

Wing Geometry MCQs : Here you will find MCQ Questions related to "Wing Geometry" in Aircraft Design. These Wing Geometry MCQ Questions Will help you to improve your Aircraft Design knowledge and will prepare you for various Examinations like Competitive Exams, Placements, Interviews and other Entrance Exmaniations




Question 1

The longest straight line that can be drawn from the Airfoil's leading edge to trailing edge is called the?

A. Mean Camber Line
B. Chord Line
C. Camber Line
D. All of the above

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Question 2

The Chord Line cuts the airfoil into an upper surface and a lower surface. If we plot the points that lie halfway between the upper and lower surfaces, we obtain a curve called the?

A. Airfoil Line
B. Camber Line
C. Mean Camber Line
D. None of the above

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Question 3

The Aspect Ratio of a wing is defined to be the square of the span divided by the wing area and is given the symbol?

A. RA
B. R
C. AsR
D. AR

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Question 4

A 3D airfoil is called _____________.

A. lofting
B. airfoil
C. engine
D. wing

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Question 5

Aspect Ratio is a measure of how long and slender a wing is from tip to tip.

A. TRUE
B. FALSE
C. Can be true or false
D. Can not say

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Question 6

The maximum distance between the upper and lower surfaces is called the?

A. Thickness
B. Thinness
C. Neither think nor thin
D. None of the above

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Question 7

A wing has root chord of 2m and taper ratio of 0.5. Determine what will be the value of tip chord?

A. 0.5
B. 1
C. 1.5
D. 2

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Question 8

If aspect ratio of wing is 8 and S=0.1m2 then, what will be the span of wing?

A. 0.89mm
B. 0.89cm
C. 0.89m
D. 0.89km

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Question 9

A positive Dihedral angle is called Anhedral?

A. TRUE
B. FALSE
C. Can be true or false
D. Can not say

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Question 10

Wing sweep is used to ____

A. increase drafting
B. decrease critical mach number
C. increase lofting
D. increase critical mach number

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