A jet aircraft is traveling at 262 m/s in hor- izontal flight. The engine takes in air at a

rate of 85.9 kg/s and burns fuel at a rate of

3.92 kg/s. The exhaust gases are ejected at

921 m/s relative to the aircraft.

Find the thrust of the jet engine.

Solution :

Speed of the air craft, = 262 m/s

Fuel burns at the rate of, = 3.92 kg/s

Rate at which the engine takes in air, = 85.9 kg/s

Speed of the exhaust gas that are ejected relative to the aircraft, =921 m/s

Therefore, the upward thrust of the jet engine is given by

F = 85.9(921 - 262) + (3.92 x 921)

   = 4862635.79 + 3610.32

   =

Therefore thrust of the jet engine is .

vapour or gas assuming atmospheriv pressure

distance = 150m

displ = root (50 ^2 + 100^2)

root(2500+10000)

root 125000