
CPL POF 5
Authored by James Douglas
Physics
Professional Development
Used 22+ times

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15 questions
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1.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
An aircraft in a level turn at a constant speed:
Is not accelerating, since its speed is steady
Is in equilibrium and thus not accelerating
Is accelerating because it is changing direction
Is at a constant velocity and is accelerating
2.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
Dynamic pressure (1/2pV2s) is obtained by:
Subtracting static pressure from total pressure
Adding static pressure and total pressure
Subtracting total pressure from pitot pressure
Measuring the pressure in the static port
3.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
The center of pressure of a cambered aerofoil:
Remains at the mid chord position over the normal operating AoA range
Moves forward as AoA increases until, when passing the stalling angle, it moves to the rear
Increases until the stalling angle and then tilts to the rear
Moves forward as airspeed increases and rearwards as it decreases
4.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
When an aerofoil is at the angle of attack for best lift/drag ratio, the total reaction is:
As near to a right angle to the relative airflow as it can be
At a right angle to the relative airflow
Parallel to the relative airflow
At a right angle to the effective airflow
5.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
The coefficient of lift incorporates the following factors:
Angle of attack, TAS, wing area
Angle of attack, shape and condition of the aerofoil
Angle of attack, density and velocity
Size and shape of the aerofoil, angle of attack
6.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
By comparison with a wing of low aspect ratio, a wing of high aspect ratio:
Produces lift more efficiently
Stalls at a higher angle of attack
Is not as efficient in producing lift
Has a lower thickness/chord ratio.
7.
MULTIPLE CHOICE QUESTION
1 min • 1 pt
Some wings are designed with washout in order to:
Prevent stalling from the wingroots first
Reduce the effects of adverse yaw
Avoid wingtip stalling
Improve lateral stability
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