Principles Of Flight Flashcards

1
Q

What is the Aerofoil section?

A

The shape of the wing from leading edge to trailing edge

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2
Q

What is the curve on the wing called?

A

The Chamber

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3
Q

What is the Angle of Attack?

A

The angle at which the wing meets the airflow

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4
Q

How is one third of the wing’s lift produced?

A

From the Angle of Attack - due to air being pushed downwards and creating an opposite effect in that the Aerofoil is pushed up

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4
Q

How is two thirds of the wing’s lift produced?

A

From the Chamber - the air has to travel a greater distance on top so travels faster and therefore the pressure on top decreases - Bernoulli’s theory

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5
Q

What is the Parallelogram of forces?

A

Where opposite forces create a resultant force, that can be calculate using trigonometry

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6
Q

What are the 4 forces during flight?

A

Weight, lift, drag and thrust

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7
Q

What does it mean when the aircraft is in equilibrium?

A

Constant height - lift equal to weight

Constant speed - thrust equal to drag

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8
Q

What are the two types of drag?

A

Induced drag

Parasite drag

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9
Q

What is induced drag?

A

Air moves outwards underneath the wing, and inwards over the top.
This causes the two air streams to meat and create trailing edge vortexes

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10
Q

What do trailing edge vortices turn into?

A

Wing-tip vortices due to them moving up towards each tip

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11
Q

How can drag be reduced?

A

By increasing the aspect ratio - (Span/Chord)

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12
Q

What are the different forms of parasite drag?

A
  • Form drag
  • Skin friction
  • Turbulence caused from additional items on the outside of plane
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13
Q

What is Total drag?

A

It includes both induced and parasite drag

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14
Q

When is parasite drag at it’s lowest?

A

At low airspeeds

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15
Q

When is induced drag at it’s lowest?

A

At high airspeeds

16
Q

What is the “speed squared law”

A

Form drag is proportional to the square of the speed

17
Q

What can the “Speed squared law” be applied to?

A

Airspeed and lift

18
Q

What does increasing the Angle of Attack cause?

A

And increase of lift and drag

19
Q

What is the critical angle of attack?

A

The angle at which the aircraft will stall - 15 degrees

20
Q

What is the stall in terms or air particles?

A

When the air no longer clings to the Aerofoil and breaks away and breaks the smooth airflow

21
Q

How can lift be created without thrust?

A

By adopting a nose-down attitude

22
Q

What is the best lift/drag ratio?

A

10:1

23
Q

What uses this ratio?

A

The best gliding angle

24
Q

What is the best gliding angle?

A

The airplane will travel 10 feet forward for every 1 foot of height loss
-60Knts

25
Q

What is minimum sink?

A

Flying at an airspeed just below the best gliding angle, this airspeed will keep you in the air the longest
-50Knts

26
Q

What is the best rate of climb?

A

To attain the maximum height in the minimum amount of time

-50Knts

27
Q

What is the best angle of climb?

A

The speed at which the rate of climb is at it’s best

-60Knts

28
Q

What is stability?

A

It is a condition which enables an aircraft to revert to it’s original flight path without pilot input

29
Q

What axis does the aircraft yaw on? + What does it cause?

A

Vertical + change of direction of heading

30
Q

What axis does the aircraft pitch on? + What does it cause?

A

Lateral + Nose up or down

31
Q

What axis does the aircraft roll on? + What does it cause?

A

Longitudinal + Banking

32
Q

How is stability archived in a rolling plane?

A

Dihedral, the angle at which the wing is from it’s roots