11.1 Flashcards

1
Q

What are the 3 axes of motion?

A

Lateral
Longitudinal
Vertical

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2
Q

Which flying controls, control movements around the lateral axis?

A

Elevators

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3
Q

What is meant by aileron lockout?

A

Ailerons lock at high speeds to keep the aircraft in control

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4
Q

What are the advantages and disadvantages of a v tail?

A

Advantages:
-weight saving

Disadvantages:

  • complex
  • Larger surface area
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5
Q

What are the secondary flying controls?

A

Lift, drag and trim devices

Flaps, slats etc.

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6
Q

What lift device gives the maximum increase in lift?

A

Fowler flap (95% increase)

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7
Q

What are trim systems used for?

A

To stabilise the aircraft so that the pilot doesn’t have to control the aircraft all the time

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8
Q

How do vortex generators reduce wave drag?

A

Transfer energy from the free-air stream to the boundary layer

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9
Q

Does the balance tab aid the pilot?

A

Yes

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10
Q

What is an anti-balance tab?

A

Tab on the wing that deflects in the same direction of the control surface to increase the efficiency of the control surface

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11
Q

What is a Mach number?

A

The speed of an aircraft in relation to the speed of sound

Speed of sound= mach 1

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12
Q

What is the critical mach number?

A

The top speed an aircraft can travel before reaching super sonic speeds

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13
Q

What wing design feature delays the onset of critical mach?

A

Swept wings

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14
Q

Where does supersonic airflow first occur on an aerofoil?

A

The trailing edge

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15
Q

What happens to air velocity in an expansion wave?

A

It increases

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16
Q

When does a bow wave form in front of the leading edge?

A

When flight speed exceeds the speed of sound

17
Q

What drag increases due to the use of vortex generators?

A

Parasite drag

18
Q

Which wing profile is also known as rear loaded?

A

A transonic profile

19
Q

What are the possible advantages of a rear loaded wing profile?

A

Increased lift

No flow separation