A civil A/C has maximum lift coefficient of 3. If wing loading is 120 – McqOptions

MCQOPTIONS

1.	A civil A/C has maximum lift coefficient of 3. If wing loading is 120 then, find approach speed of the aircraft. Consider sea-level density.
A.	10.5m/s
B.	10.50km/s
C.	12
D.	120
Answer» B. 10.50km/s

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+0.02CL2 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.
Following graph represents __________
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.
A civil A/C has maximum lift coefficient of 3. If wing loading is 120 then, find approach speed of the aircraft. Consider sea-level density.
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.