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Aircraft Technic
#1. The imaginary straight line which passes through an aerofoil section from leading edge to trailing edge is called
#2. Wing tip vortices create a type of drag known as
#3. As the angle of attack is increased (up to the stall point), which of the following is correct?
#4. When an aircraft is in straight and level unaccelerated flight, which of the following is correct?
#5. When air flow velocity over an upper cambered surface of an aerofoil decreases, what takes place?
#6. With an increase in altitude under I.S.A. conditions the temperature in the troposphere
#7. Stability of an aircraft is
#8. With reference to altimeters QFE is
#9. ................................. set the center of gravity to the effective position. (by transferring fuel from the trim tank to the wings or opposite)
#10. Under the ICAO “Q” code there are which three settings?
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To see more aerodynamic questions:
Aerodynamic Quiz 1
Aerodynamic Quiz 2
Aerodynamic Structure Quiz