An aircraft with a cruising speed of 750 km / h, at an altitude of about 11500 m. is progressing. The aircraft has a top view area of 160 m2 and a total mass of 80000 kg. given. Also, the air density at this altitude is about 0.3 kg/ms. airplane landing and uses double-slit wings for take off. However, while cruising It continues its flight by collecting its wings. NACA 23012 airfoil own aircraft; a) at the time of take-off and landing when the wings are extended and not extended Find the safe lowest speeds required. b) determine the angle of attack required for continuous cruise at cruise altitude. c) the strength to provide the necessary thrust to overcome the resistance force coming upon it. calculate. (Air density on the ground is determined as 1.20 kg/m3.
An aircraft with a cruising speed of 750 km / h, at an altitude of about 11500 m.
is progressing. The aircraft has a top view area of 160 m2 and a total mass of 80000 kg.
given. Also, the air density at this altitude is about 0.3 kg/ms. airplane landing
and uses double-slit wings for take off. However, while cruising
It continues its flight by collecting its wings. NACA 23012 airfoil
own aircraft;
a) at the time of take-off and landing when the wings are extended and not extended
Find the safe lowest speeds required.
b) determine the angle of attack required for continuous cruise at cruise altitude.
c) the strength to provide the necessary thrust to overcome the resistance force coming upon it.
calculate.
(Air density on the ground is determined as 1.20 kg/m3.
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