
Quiz on Aerodynamics and Angle of Attack
Authored by Kathryn Cadman
Engineering
12th Grade
Used 2+ times

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16 questions
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1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the angle of attack?
The angle between the wing and the ground
The angle between the aircraft and the horizon
The angle between the chord line of an aerofoil and the undisturbed, relative airflow
The angle between the wing and the tail of the aircraft
Answer explanation
The angle of attack is defined as the angle between the chord line of an aerofoil and the undisturbed, relative airflow. This is crucial for understanding lift generation in aerodynamics.
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What happens when the angle of attack exceeds the critical angle?
The aircraft gains more lift
The wing stalls
The drag force is eliminated
The aircraft speeds up
Answer explanation
When the angle of attack exceeds the critical angle, the airflow over the wing becomes turbulent, causing a loss of lift and resulting in a stall. Therefore, the correct answer is that the wing stalls.
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the effect of lowering the flaps on a wing?
It decreases the drag force
It increases the lift coefficient
It reduces the surface area of the wing
It decreases the camber of the wing
Answer explanation
Lowering the flaps increases the lift coefficient by enhancing the wing's camber and increasing the effective surface area, allowing the wing to generate more lift at lower speeds.
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the primary cause of lift on a wing?
The wing's weight is reduced
The wing's speed is increased
The static pressure above the wing is greater than below
The static pressure below the wing is greater than above
Answer explanation
Lift is primarily generated because the static pressure below the wing is greater than above. This pressure difference creates an upward force, allowing the wing to rise.
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the center of pressure (CP)?
The point where the maximum lift is generated
The point where the drag force is minimized
The point where the total aerodynamic reaction force acts
The point where the total weight of the aircraft acts
Answer explanation
The center of pressure (CP) is the point where the total aerodynamic reaction force acts on an aircraft. This point is crucial for stability and control, as it influences how the aircraft responds to aerodynamic forces.
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the effect of increasing the angle of attack on lift?
Lift remains constant
Lift decreases
Lift increases
Lift becomes zero
Answer explanation
Increasing the angle of attack enhances the airflow over the wings, leading to greater lift until a critical angle is reached. Therefore, the correct answer is that lift increases.
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the role of camber in a wing?
It decreases the lift coefficient
It reduces the wing's surface area
It increases the drag force
It increases the lift coefficient
Answer explanation
Camber is the curvature of a wing, which helps to increase the lift coefficient by altering the airflow over the wing. This enhanced lift is crucial for better performance during flight.
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