Dale Crane Q's Flashcards
Two variables in the angle of attack of a propeller are:
- engine RPM (rotational speed)
- Forward velocity (speed of aircraft)
The curved surface of a propeller blade is the ______
(back or face)
back
The pitch angle and the angle of attack of a propeller blade _______ the same.
(are or are not)
are not
(would only be the same if no forward velocity)
Propeller blade stations are measured in inches from the _______ (hub or tip)
hub
The actual distance a propeller advances in one revolution in theair is the _________ pitch
(effective or geometric)
effective
The difference between the geometric and effective pitch of a propeller is called _____
slip
Five factors that affect the amount of thrust produced by a propeller blade are:
- Airfoil shape
- Air density
- Angle of Attack
- Velocity of airflow
- Area of airfoil
Two things that change on a propeller blade from the root to the tip are:
- Blade pitch angle
- Cross section of the blade
Increasing the engine RPM with the forward speed remaining constant _________ the angle of attack
(increases or decreases)
increases
Five forces acting on a propeller turning at a high speed are:
- Centrifugal force
- Thrust bending force
- Torque bending force
- Aerodynamic twisting force
- Centrifugal twisting force
The greatest force acting on a propeller is _______ force
centrifugal
The force that tries to bend a propeller blade forward is the _____ bending force
thrust
The force that tries to bend a propeller blade in its plane of rotation is the ___________ force
Torque bending force
Aerodynamic twisting force (ATF) tries to _______ the blade angle
(increase or decrease)
increase
Centrifugal twisting force (CTF) tries to ______ the blade angle
(increase or decrease)
decrease