Determine wing loading for civil aircraft if lift-off speed is 80m/s a – McqOptions

MCQOPTIONS

1.	Determine wing loading for civil aircraft if lift-off speed is 80m/s and maximum lift coefficient is 2.8.
A.	9071.07
B.	9111
C.	911
D.	91
Answer» B. 9111

Discussion

No Comment Found

Related MCQs

A prop driven A/C has BHP/W as 0.08. If density ratio is 0.2 and take off lift coefficient is 3 then find take-off parameter for the aircraft. Given wing loading W/s = 35.
Jet aircraft with CD=0.01+0.02CL<sup>2</sup> is performing loiter. Find wing loading for maximum loiter if, AR=8.5, e=0.7 and dynamic pressure is 25Pa.
Which of the following is correct for maximum jet range?
For prop aircraft at maximum range what will be the wing loading. Given CD0=0.02, aspect ratio as 8, e=0.6 and q=39.20Pa.
An aircraft has catapult end speed of 30m/s and wind over deck as 20m/s. If maximum CL is 2.6 and density is 1.22 then, find catapult wing loading.
Which of the following is correct for a jet aircraft take-off parameter (TOP)?
Determine wing loading for civil aircraft if lift-off speed is 80m/s and maximum lift coefficient is 2.8.
An aircraft is flying with wing loading of 50 and maximum CL as 2.4. If density is 1.225 then, find the stall speed of the aircraft.
As a designer I want to reduce the empty weight of my aircraft. Therefore I will ______
Low wing loading will provide ___________