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POF - Propellers

Authored by Talya Morgan

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University

Used 28+ times

POF - Propellers
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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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