1-111

1-111

University

110 Qs

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1-111

1-111

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110 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How does the aileron control the roll of an aircraft?

By changing the angle of attack on each wing

By changing the speed of the aircraft

By altering the shape of the fuselage

By shifting the center of gravity

By adjusting the throttle

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following describes a laminar flow of air?

Turbulent airflow with swirls and eddies

Smooth, streamlined airflow over the aircraft's surface

Airflow that causes drag at high speeds

Airflow that generates lift over the wing

Airflow that occurs when the aircraft is stalled

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What happens to the lift produced by an aircraft wing as the angle of attack increases?

Lift fluctuates randomly

Lift decreases

Lift remains the same

Lift increases

Lift becomes zero

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What type of stability describes an aircraft that naturally returns to its original flight path after being disturbed?

Positive stability

Negative stability

Neutral stability

Dynamic stability

Longitudinal stability

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following best describes the relationship between airspeed (TAS) and lift?

Lift is independent of airspeed

Lift decreases with the square of the airspeed

Lift increases with the square of the airspeed

Lift increases linearly with airspeed

Lift decreases linearly with airspeed

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the rudder in an aircraft?

To control the yaw of the aircraft

To control the pitch of the aircraft

To control the roll of the aircraft

To increase the lift produced by the wings

To increase the drag on the aircraft

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In which of the following situations does a wing produce the maximum lift?

At a high altitude

At a low angle of attack

At a high angle of attack

When the airspeed is zero

At the critical angle of attack

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