Total thrust output by both engines =
Average drag = 28657 N
Mass of plane = 156892 kg
By Newton's 2nd law,
Thrust - Drag = M*a
193536 - 28657 = 156892*a
Acceleration , a = 1.050908 m/s2
(for constant acceleration) change in speed = a * t
Change in speed = 850 - 739.64 = 110.36 km/h = (2759/90) m/s = 30.655556 m/s
Time it takes to reach new speed = change in speed / a = 29.1705 s
Boeing 767-400ER model airplane has two engines. Each engine can have a maximum thrust (mechanical force)...
Boeing 767-400ER model airplane has two engines. Each engine can have a maximum thrust (mechanical force) output of 270 kN. When the plane is cruising at 749.77 km/h, the pilot decides to increase the speed to the typical 850.0 km/h. If drag on the plane is on average 25556 N, and the engines are engaged at 35.21 % of their maximum thrust output, and the plane weighs 128256 kg, how long does it take to reach the new cruising speed?...
Consider a large jet airplane which has the following characteristics: Maximum gross weight = 130000 N General • Fuel weight = 50000 N Wing 2 Wing area = 50 m Wing aspect ratio (AR) = 6.5 Wing span efficiency factor (e) = 0.87 Aerodynamics . = MARE • Zero-lift drag coefficient = 0.032 Drag Cp = Cpo + kc where k = kı + kz kı = 0 and k3 Lift CLmax = 1.4 during flight Two turbojet engines. (thrust...