An aircraft is designed to have landing weight of 2500N and stall spee – McqOptions

MCQOPTIONS

1.	An aircraft is designed to have landing weight of 2500N and stall speed V of 9.8m/s. How much kinetic energy should be absorbed by wheel? Consider number of wheels with brake is 2.
A.	6125J
B.	5.98 KJ
C.	2100
D.	235 KJ
Answer» B. 5.98 KJ

Discussion

No Comment Found

Related MCQs

If tire pressure is 25 psi then, determine minimum dynamic hydroplaning speed.
Determine weight carried by wheel if inflation pressure is 100 psi and footprint area is 80 inch<sup>2</sup>.
An aircraft is designed to have landing weight of 2500N and stall speed V of 9.8m/s. How much kinetic energy should be absorbed by wheel? Consider number of wheels with brake is 2.
An aircraft has weight of 300N at the time of landing. Calculate braking K.E. if stall speed is 10 m/s.
Jet fighter aircraft is designed to operate from rough unpaved runway. Find the diameter of wheel if wheel needs to carry weight of 200 unit.
A twin business engine is designed in such way that the load of 250 unit is carried out by the tire. Find the appropriate ratio of the diameter to the width of main wheel.
Evaluate width of the wheel if weight carried by it is 200 unit. Consider general aviation aircraft.
Only dynamic loading should be used for determining the nose wheel tire sizing.
A general aviation aircraft has impact Weight on wheel about 100 unit. Find the required diameter.