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A small airplane with a wingspan of 10 m is flying at a speed of 72 km/h. The difference in air pressure below and above the wings is measured to be 500 Pa. Assuming the lift force is entirely due to the pressure difference and acts perpendicular to the wings, what is the mass of the airplane? (Take air density as 1.2 kg/m³)
1020 kg
1200 kg
Cannot be determined without the wing area. If the wing area is 'A' m², then the mass is 51.02*A kg.
1500 kg
An aircraft is flying at a constant altitude and velocity. Which of the following statements is INCORRECT regarding the lift generated by its wings?
The lift generated is equal to the weight of the aircraft.
The lift coefficient remains constant.
The angle of attack remains constant.
The lift generated is directly proportional to the square of the angle of attack.
How does the velocity of air over the top surface of a wing generating lift compare to the velocity of air under the bottom surface?
The velocity over the top surface is significantly higher.
The velocity under the bottom surface is significantly higher.
The velocities are approximately equal.
The velocity difference is negligible for lift generation.
Which principle is fundamentally responsible for the dynamic lift experienced by an airplane wing?
Bernoulli's principle
Archimedes' principle
Pascal's law
Newton's third law
The shape of an airplane wing is designed such that the airspeed is ____ over the top surface compared to the bottom surface.
higher
lower
equal
unpredictable
Dynamic lift is primarily dependent on the ______ of the airflow.
speed
density
temperature
humidity
If the airspeed above an airplane wing is increased, the pressure above the wing will:
decrease
increase
remain the same
fluctuate randomly