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Question 76-1 : Propellers and rotors. lift generated by a blade depends on.1 airmass density.2 relative wind speed.3 blade area.4 blade's angle of attack.5 airfoil shape ? [ Mandatory specific ]

1, 2, 3, 4, 5.

exemple 76 1, 2, 3, 4, 5.

Question 76-2 : Propellers & rotors. the diameter of a propeller blade is usually expressed in ?

Inche.

exemple 80 Inche.

Question 76-3 : Propellers & rotors. the pitch of a propeller blade is usually expressed in ?

Inche.

exemple 84 Inche.

Question 76-4 : Propellers & rotors. the geometric pitch of a propeller is the ?

Distance a propeller blade element is travelling in forward direction in one propeller revolution.

exemple 88 Distance a propeller blade element is travelling in forward direction in one propeller revolution.

Question 76-5 : Propellers and rotors. propeller efficiency may be defined as the ratio between ?

Power available / power required.

exemple 92 Power available / power required.

Question 76-6 : Propellers and rotors. a propeller blade is twisted, so as to ?

Equalize the lift over the entire length of the blade.

exemple 96 Equalize the lift over the entire length of the blade.

Question 76-7 : The statement that best describes the effect of the center of gravity on the aircraft stability is ?

A forward center of gravity increases the natural stability of an aircraft.

exemple 100 A forward center of gravity increases the natural stability of an aircraft.

Question 76-8 : Indicate how the conventional multicopter controls its attitude ?

The engines change their rotational speed rpm according to the desired direction of flight.

exemple 104 The engines change their rotational speed (rpm) according to the desired direction of flight.

Question 76-9 : The ground effect ?

Reduces induced drag.

exemple 108 Reduces induced drag.

Question 76-10 : The laminar layer on a wing profile is ?

The thin, smooth flow on the extrados, from the leading edge to the point of transition.

exemple 112 The thin, smooth flow on the extrados, from the leading edge to the point of transition.

Question 76-11 : The turbulent layer on a wing profile is ?

The thick and turbulent flow on the extrados, after the point of transition.

exemple 116 The thick and turbulent flow on the extrados, after the point of transition.

Question 76-12 : The imaginary line joining the leading and trailing edge of the wing is called ?

Cord line.


Question 76-13 : The part of the wing, shown by the arrow, is. 55 ?

A flap.


Question 76-14 : Spoiler extension for a fixed wing drone causes ?

An increase in drag and decrease in lift.


Question 76-15 : Induced drag is associated with ?

Lift.



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