
CPL PoF propeller revision
Authored by Needs Remedial
Specialty, Other
Professional Development
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20 questions
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1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The propeller is a rotating aerofoil:
True
False
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Blade angle is:
Angle between the chord line and the plane of rotation
Angle between the blade back and the plane of rotation
Angle between the chord line and RAF
Angle between the RAF and the blade back
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The blade face is:
The side of the propeller blade facing away from the pilot
The side of the propeller blade facing toward the pilot
The leading edge of the propeller
Where the blade and the spinner meet
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The angle between the RAF and the plane of rotation is known as:
AoA
Blade angle
Helix Angle
Angle of incidence
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the purpose of helical twist?
A reduction in blade angle towards the propeller tip to maintain best thrust/torque ratio
An increase in blade angle towards the propeller tip to maintain best thrust/torque ratio
A reduction in blade angle towards the propeller tip to maintain 16° AoA for the entire blade length
An increase in blade angle towards the propeller tip to 16° AoA for the entire blade length
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The most useful thrust is produced at approximately:
50% to blade radius
25% blade radius
75% blade radius
The entire blade radius assuming the propeller is twisted to maintain best AoA
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
An aircraft with a fixed pitch propeller is cruising at 120 knots and best cruise rpm. If the speed is increase without changing RPM what will happen to the AoA and efficiency of the propeller?
AoA will decrease and efficiency will increase
AoA will increase and efficiency will increase
AoA will decrease and efficiency will decrease
AoA will increase and efficiency will increase
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