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Module 6: Aircraft Performance & Design - Quiz

Total questions: 85

Worksheet time: 43mins

Name
Class
Date
1.

What is shown in the bottom right image of the learning material?

a)

A small airplane flying over land and water

b)

A bird flying in the sky

c)

A rocket launching

d)

A helicopter landing

2.

What is the main topic of Module 6 in the learning material?

a)

Configuration Design

b)

Longitudinal Stability

c)

Role of the Tail

d)

Aerodynamic Centre

3.

Which topic is covered in Topic 3 of Module 6?

a)

Longitudinal Stability

b)

Aerodynamic Centre

c)

Summary & Questions

d)

How to Make a Stable Aircraft

4.

What is compared in the introduction of this module?

a)

Aerodynamic Centre vs Centre of Pressure

b)

Longitudinal Stability vs Lateral Stability

c)

Role of the Tail vs Role of the Wing

d)

PME vs Centre of Gravity

5.

What is one use of the PME mentioned in the module?

a)

Longitudinal Stability

b)

Making a paper airplane

c)

Flying a kite

d)

Painting an aircraft

6.

What is the role of the tail in an aircraft, according to the module?

a)

To help make a stable aircraft

b)

To make the aircraft faster

c)

To decorate the aircraft

d)

To carry passengers

7.

What is the aerodynamic centre of an aerofoil?

a)

The point where the pitching moment about CG due to angle of attack is zero.

b)

The point where the total lift is maximum.

c)

The point where the airspeed is highest.

d)

The point where the wing is thickest.

8.

What does the centre of pressure represent on an aerofoil?

a)

The point where the total sum of pressure distributed over the aerofoil acts.

b)

The point where the air is calmest.

c)

The point where the wing bends.

d)

The point where the engine is attached.

9.

Which symbol in the diagram represents the aerodynamic centre?

a)

Green dot

b)

Blue star

c)

Red arrow

d)

Black circle with cross

10.

If you want to find the point where the resultant force acts on an aerofoil, which centre should you look for?

a)

Centre of pressure

b)

Aerodynamic centre

c)

CG position

d)

Wing tip

11.

Why is the aerodynamic centre important for an aerofoil?

a)

It is where the pitching moment about CG due to angle of attack is zero.

b)

It is where the wing is painted.

c)

It is where the passengers sit.

d)

It is where the engine is located.

12.

What is the neutral point (np) of an aircraft better known as?

a)

The moving point of the aircraft

b)

The fixed aerodynamic centre of the aircraft

c)

The tail of the aircraft

d)

The wing of the aircraft

13.

In the simplified analogy, what is the tail's contribution to lift lumped into?

a)

The wing force

b)

The pitching moment only

c)

The camber moment

d)

The resultant aerodynamic force

14.

Which force is shown acting upwards from the wing in the diagram?

a)

Force due to Tail

b)

Resultant Aerodynamic Force

c)

Force due to Wing

d)

Moment due to Camber

15.

What does the whole aircraft model analogy help with?

a)

Making the aircraft fly faster

b)

Easing performance modelling

c)

Painting the aircraft

d)

Making the aircraft heavier

16.

What is the pitching moment of a zero-lift aircraft mainly produced by?

a)

The zero-lift moment due to wing camber and the tail

b)

The engine power and the wheels

c)

The color of the aircraft and the windows

d)

The number of seats and the doors

17.

Which part of the aircraft can still produce lift and a pitching moment even when there is no net lift force from the wing?

a)

The tail

b)

The wheels

c)

The cockpit

d)

The propeller

18.

What does the diagram with the airplane and arrows show?

a)

How forces and moments act on a zero-lift aircraft

b)

How to land an airplane

c)

How to paint an airplane

d)

How to open the airplane door

19.

Why can an aircraft have a pitching moment even when the net lift force is zero?

a)

Because of the wing camber and the tail

b)

Because of the color of the plane

c)

Because of the number of passengers

d)

Because of the shape of the windows

20.

What is the neutral point of an aircraft also called?

a)

The aerodynamic centre

b)

The tail

c)

The wing tip

d)

The cockpit

21.

What must we assume about the aerodynamic force due to angle of attack in the equivalent aircraft model?

a)

It is created wholly by the wing

b)

It is created by the tail only

c)

It is created by the engine

d)

It is created by the landing gear

22.

What happens to the tail effects in the equivalent aircraft model?

a)

They are wrapped up in the Aircraft Zero-Lift Moment

b)

They are ignored

c)

They are doubled

d)

They are moved to the cockpit

23.

Which point on the airplane diagram is marked with a star?

a)

Neutral point

b)

Cockpit

c)

Tail

d)

Wing tip

24.

What is the main topic discussed in this section?

a)

Longitudinal Stability

b)

Weather Patterns

c)

Types of Engines

d)

Air Traffic Control

25.

What is one use of the pitching moment equation mentioned in the material?

a)

Stability Explanation

b)

Fuel Calculation

c)

Passenger Counting

d)

Weather Forecasting

26.

Which type of aircraft is mentioned in the material?

a)

Stable Aircraft

b)

Fast Aircraft

c)

Large Aircraft

d)

Old Aircraft

27.

Why might someone use the pitching moment equation according to the material?

a)

To explain stability

b)

To find lost luggage

c)

To book tickets

d)

To paint the aircraft

28.

What does PME stand for in the context of the image?

a)

Pitching Moment Equation

b)

Perfect Motion Equation

c)

Plane Movement Equation

d)

Primary Motion Equation

29.

Which of the following is one use of the Simplified Pitching Moment Equation?

a)

Tail Lift for Trim

b)

Engine Thrust Calculation

c)

Fuel Efficiency

d)

Wing Color Selection

30.

What is the Neutral Point used for, according to the image?

a)

Useful in Aircraft Design

b)

Useful in Cooking

c)

Useful in Car Repair

d)

Useful in Painting

31.

If you want to know about Static Margin, which equation would you use based on the image?

a)

Simplified Pitching Moment Equation

b)

Simplified Thrust Equation

c)

Simplified Drag Equation

d)

Simplified Lift Equation

32.

Why is Tail Lift for Trim important in aircraft performance?

a)

It helps keep the airplane balanced.

b)

It changes the airplane's color.

c)

It makes the airplane go faster.

d)

It helps the airplane land in water.

33.

What does stability in mechanics refer to?

a)

The tendency of a rigid body to return to equilibrium after a disturbance

b)

The speed of an object

c)

The color of an object

d)

The size of an object

34.

How many types of stability are there?

a)

One

b)

Two

c)

Three

d)

Four

35.

Which of the following is NOT a type of stability mentioned in the material?

a)

Positive stability

b)

Neutral stability

c)

Negative stability

d)

Rotational stability

36.

In aircraft, what determines stability?

a)

The color of the aircraft

b)

The position of the centre of gravity relative to the centre of lift

c)

The number of passengers

d)

The type of fuel used

37.

Why is it important to learn about how aircraft design influences stability?

a)

To know how to paint an aircraft

b)

To understand why stability is important for safe flight

c)

To learn how to make aircraft faster

d)

To find out how to make aircraft heavier

38.

Match the drawing to the 'type' of stability shown in the diagram.

a)

Positive stability, Neutral stability, Negative stability

b)

Negative stability, Positive stability, Neutral stability

c)

Neutral stability, Negative stability, Positive stability

d)

Positive stability, Negative stability, Neutral stability

39.

What does a simple weather vane always do when the wind changes direction?

a)

It points into the wind.

b)

It falls to the ground.

c)

It spins in circles.

d)

It stops moving.

40.

What can cause an aircraft to face a change in wind direction?

a)

A gust of up- or down-moving air.

b)

A flat tire.

c)

A broken engine.

d)

A sunny day.

41.

What does a stable aircraft do when there is a disturbance to its equilibrium?

a)

It acts like a weather vane and returns to its original position.

b)

It falls out of the sky.

c)

It speeds up very fast.

d)

It stops moving.

42.

Look at the diagram showing the weathercock analogy. What does the final position of the weather vane show?

a)

The weather vane points into the wind after being disturbed.

b)

The weather vane breaks apart.

c)

The weather vane spins forever.

d)

The weather vane points away from the wind.

43.

What happens to the aircraft's centre of pressure when the angle of attack changes?

a)

It stays in the same place

b)

It shifts

c)

It disappears

d)

It becomes the centre of gravity

44.

Where is the centre of pressure when the aircraft is trimmed?

a)

On the centre of gravity

b)

At the tip of the wing

c)

At the tail of the aircraft

d)

Under the aircraft

45.

What is the centre of pressure the locus of?

a)

The aircraft’s total lift

b)

The aircraft’s speed

c)

The aircraft’s weight

d)

The aircraft’s fuel

46.

When the angle of attack increases, what happens to the centre of pressure in a stable aircraft?

a)

It shifts forward

b)

It shifts back

c)

It stays the same

d)

It moves to the tail

47.

If the angle of attack decreases, what does the centre of pressure do in a stable aircraft?

a)

Shifts forward

b)

Shifts back

c)

Disappears

d)

Moves to the wingtip

48.

Why is there no moment when the aircraft is trimmed?

a)

Because the centre of pressure is on the centre of gravity

b)

Because the aircraft is flying upside down

c)

Because the wings are flat

d)

Because the engine is off

49.

What does a restoring moment do in a stable aircraft?

a)

Helps the aircraft return to its trimmed position

b)

Makes the aircraft go faster

c)

Turns the aircraft upside down

d)

Stops the aircraft from flying

50.

What is the centre of pressure in an aircraft?

a)

The place where the aircraft's total lift acts

b)

The place where the aircraft's total weight acts

c)

The place where the aircraft's engine is located

d)

The place where the aircraft's fuel is stored

51.

When the aircraft is trimmed, where is the centre of pressure located?

a)

On the centre of gravity

b)

On the wingtip

c)

On the tail

d)

On the nose

52.

What happens to the centre of pressure when the angle of attack changes?

a)

It shifts

b)

It disappears

c)

It stays in the same place

d)

It moves to the tail

53.

Why is there no moment when the centre of pressure is on the centre of gravity?

a)

Because the forces are balanced

b)

Because the aircraft is upside down

c)

Because the engine is off

d)

Because the wings are folded

54.

If the angle of attack increases in a stable aircraft, what happens to the centre of pressure?

a)

It shifts back, restoring moment

b)

It shifts forward, causing a spin

c)

It stays in the same place

d)

It moves to the tail and stays there

55.

If the angle of attack decreases in a stable aircraft, what happens to the centre of pressure?

a)

It shifts forward, restoring moment

b)

It shifts back, causing a stall

c)

It stays in the same place

d)

It moves to the wingtip

56.

What does the green dot represent in the diagram?

a)

Centre of pressure

b)

Centre of gravity

c)

Engine

d)

Tail

57.

What does the black-and-white circle represent in the diagram?

a)

Centre of gravity

b)

Centre of pressure

c)

Wingtip

d)

Cockpit

58.

What happens when a stable aircraft encounters rising air?

a)

The aircraft increases its angle of attack (AoA)

b)

The aircraft decreases its angle of attack (AoA)

c)

The aircraft stops moving

d)

The aircraft flies upside down

59.

What does a stable aircraft do after it encounters rising or descending air?

a)

It rotates back to its original angle of attack

b)

It keeps flying in the new direction forever

c)

It lands immediately

d)

It spins in circles

60.

When a stable aircraft encounters descending air, what happens to the total force locus?

a)

It moves forward

b)

It moves backward

c)

It disappears

d)

It stays in the same place

61.

Why does a restoring moment get produced in a stable aircraft?

a)

To help the aircraft return to its original angle of attack

b)

To make the aircraft go faster

c)

To make the aircraft stop

d)

To make the aircraft fly upside down

62.

What is the neutral point of an aircraft also called?

a)

The aerodynamic centre

b)

The tail

c)

The wing

d)

The cockpit

63.

What does the moment due to camber represent in an aircraft?

a)

The pitching moment created by the tail and wing camber when total lift is zero

b)

The speed of the aircraft

c)

The color of the aircraft

d)

The number of passengers

64.

Which force acts at the neutral point of an aircraft?

a)

Resultant Aerodynamic Force

b)

Gravity

c)

Engine Thrust

d)

Friction

65.

What does the star symbol in the second airplane diagram represent?

a)

Neutral point

b)

Engine

c)

Wing tip

d)

Landing gear

66.

If the total lift of an aircraft is zero, what is the moment due to camber similar to?

a)

The pitching moment created by the tail and wing camber

b)

The speed of the aircraft

c)

The color of the aircraft

d)

The number of seats

67.

What does the analytical explanation help with?

a)

It is more convenient to the maths

b)

It is easier to understand

c)

It is only about the tail

d)

It ignores the main wing

68.

What do we ignore during a perturbation according to the simplification?

a)

Any extra production of lift from the tail

b)

The main wing

c)

The centre of gravity

d)

The neutral point

69.

Where is all the aircraft CL produced according to the simplification?

a)

By the main wing

b)

By the tail

c)

By the centre of gravity

d)

By the neutral point

70.

What is the neutral point also called?

a)

Aerodynamic centre

b)

Centre of gravity

c)

Main wing

d)

Tail

71.

What does the neutral point represent?

a)

The locus of the lift due to angle of attack

b)

The centre of gravity

c)

The tail of the aircraft

d)

The main wing

72.

What happens when there is a positive change in angle of attack (AoA)?

a)

Lift force increases, restoring moment

b)

Lift force decreases, restoring moment

c)

The tail produces more lift

d)

The centre of gravity moves

73.

What happens when there is a negative change in angle of attack (AoA)?

a)

Lift force decreases, restoring moment

b)

Lift force increases, restoring moment

c)

The main wing disappears

d)

The neutral point moves

74.

What happens when a stable aircraft encounters rising air?

a)

The aircraft increases its angle of attack (AoA).

b)

The aircraft stops moving.

c)

The aircraft decreases its angle of attack (AoA).

d)

The aircraft flies upside down.

75.

What is produced when a stable aircraft encounters either rising or descending air?

a)

Restoring moment

b)

Loud noise

c)

Engine failure

d)

Lightning

76.

If a stable aircraft encounters descending air, what happens to its angle of attack (AoA)?

a)

The angle of attack decreases.

b)

The angle of attack increases.

c)

The angle of attack stays the same.

d)

The aircraft lands immediately.

77.

Why does a stable aircraft return to its original angle of attack after encountering rising or descending air?

a)

Because a restoring moment is produced.

b)

Because the pilot turns off the engine.

c)

Because the wings fall off.

d)

Because it runs out of fuel.

78.

What happens to the aircraft when there is an up-gust?

a)

The aircraft experiences a positive change in lift coefficient.

b)

The aircraft experiences a negative change in lift coefficient.

c)

The aircraft does not change at all.

d)

The aircraft stops moving.

79.

What does a negative change in pitching moment coefficient cause in the aircraft?

a)

Nose-up moment

b)

Nose-down moment

c)

The aircraft flies faster

d)

The aircraft lands

80.

What does the subsequent motion do after an up-gust affects the aircraft?

a)

Makes the aircraft fly higher

b)

Restores the aircraft to original

c)

Makes the aircraft turn left

d)

Stops the aircraft

81.

If the tail of the aircraft is producing 'negative' lift at zero lift, what does this help to achieve?

a)

Makes the aircraft go faster

b)

Makes the aircraft stable

c)

Makes the aircraft heavier

d)

Makes the aircraft land

82.

What happens to the aircraft's nose when there is a positive change in pitching moment due to an up-gust?

a)

The nose goes up

b)

The nose goes down

c)

The wings fall off

d)

The aircraft stops moving

83.

What does a positive change in the lift coefficient due to an up-gust cause in an unstable aircraft?

a)

A nose-up moment

b)

A nose-down moment

c)

The aircraft slows down

d)

The aircraft lands

84.

According to the diagram, what happens to the motion of an unstable aircraft after an up-gust?

a)

The motion diverges away from the original position

b)

The motion returns to the original position

c)

The aircraft stops in the air

d)

The aircraft flies in circles

85.

If the tail of the aircraft is producing positive lift at zero lift, what does this mean for the pitching moment at zero lift?

a)

The pitching moment would be negative

b)

The pitching moment would be zero

c)

The pitching moment would be positive

d)

The aircraft would not fly