Wing aspect ratio is defined as _____ – McqOptions

MCQOPTIONS

1.	Wing aspect ratio is defined as _____
A.	span square divided by reference area
B.	span square multiplied by reference area
C.	span square plus reference area
D.	span square
Answer» B. span square multiplied by reference area

Discussion

No Comment Found

Related MCQs

A twin turboprop engine is flying with 120m/s. Wing of the aircraft has span of 2m and lift co-efficient as 0.15 with aspect ratio as 9.2. Find the lift produced by the wing.
Determine the corrections or otherwise of the following assertion [A] and reason [R]:<br>Assertion [A]: Taper ratio will affect the weight of wing.
A jet fighter is operating at Mach number of 1.4. Wing chord is 1m then, find the location of aerodynamic centre.
If a sailplane is to be designed then, the aspect ratio of the sailplane will be ______
A typical wing has aspect ratio of 7 and span of 2m. If taper ratio T = 0.2 then, find the value of root chord.
Wing aspect ratio is defined as _____
Wing planform is affected by _____
A wing has root chord of 2m and taper ratio of 0.5. Determine what will be the value of tip chord?
If taper ratio is T and span is b with surface area as S then the root chord is _____
Wing and airfoil both are 3D phenomena.