POF - Propellers

POF - Propellers

University

20 Qs

quiz-placeholder

Similar activities

3: Aero Engines

3: Aero Engines

University

15 Qs

Circular Saw Safety Quiz

Circular Saw Safety Quiz

University

21 Qs

RPL Aerodynamics Section 1-8 Questions

RPL Aerodynamics Section 1-8 Questions

University

24 Qs

Aircraft Stresses and Basic Aerodynamics

Aircraft Stresses and Basic Aerodynamics

University

15 Qs

Aviation

Aviation

5th Grade - University

25 Qs

Survey Camp Hydro - Set 2

Survey Camp Hydro - Set 2

University

19 Qs

ME8561_UNIT-III_MCQ

ME8561_UNIT-III_MCQ

University

25 Qs

POF - Propellers

POF - Propellers

Assessment

Quiz

Other

University

Hard

Created by

NZAAL Theory

Used 15+ times

FREE Resource

20 questions

Show all answers

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

Create a free account and access millions of resources

Create resources
Host any resource
Get auto-graded reports
or continue with
Microsoft
Apple
Others
By signing up, you agree to our Terms of Service & Privacy Policy
Already have an account?