Quiz on Aerodynamics and Angle of Attack

Quiz on Aerodynamics and Angle of Attack

12th Grade

16 Qs

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Quiz on Aerodynamics and Angle of Attack

Quiz on Aerodynamics and Angle of Attack

Assessment

Quiz

Engineering

12th Grade

Easy

Created by

Kathryn Cadman

Used 1+ times

FREE Resource

16 questions

Show all answers

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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