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Aeroplanlære - Kap 2 (Basics) Flashcards

1
Q

When is the only time an aircraft can become and stay airborne?

A

When it does work on the air to produce a force to oppose gravity

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2
Q

Why do wings work according to newtons law?

A

Because they are driven through the air at a speed that allows them to oppose gravity

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3
Q

Why do we use a propeller?

A

To provide at least a an equal and opposite force to oppose drag

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4
Q

Describe the forces that works on an aircraft

A
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5
Q

Which 2 methods does a wing have to create force?

A

Flat plate lift
Differential pressure effect

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6
Q

How does flat plate lift work?

A

A flat surface is angled so that is pushes air down and creates and opposing force upwards

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7
Q

How does differential pressure effect work?

A

The shape of the wing creates a low pressure on top of the wing and a high pressure underneath, this “sucks” the wing up

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8
Q

When does differential pressure effect work on an object?

A

When the object is:
1. Curved
2. Has a curved leading edge
3. Has a sharp trailing edge
4. Is set to a relatively low angle to the airflow

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9
Q

What is the requirement for an aerofoil?

A

A relatively smoothly curved leading edge
An upper surface that is convex
A sharp trailing edge

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10
Q

Describe the pressure around an aerofoil

A
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11
Q

What is absolutely critical to produce a low pressure above an aerofoil?

A

An angle of attack
(Maximum around 16°)

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12
Q

What is the effect that bends the air over the wing called?

A

Coanda effect

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13
Q

What happens to the air at an angle of attack exceeding 16°?

A

The air breaks away

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14
Q

What are the two concepts fundamental to an understanding of the properties and behavior of flowing air?

A

The equation of continuity and bernoulli’s theorem

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15
Q

What is the basic assumptions of an ideal fluid?

A

Incompressible - This is approximately true for flight at slower speeds
Has no viscosity

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16
Q

What is the equation of continuity?

A

Mass can neither be created nor destroyed

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17
Q

Is mass flow a constant value?

A

Yes

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18
Q

When mass flow is put through a venturi tube, what is constant at all points?

A

The density of the air

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19
Q

What happens to the velocity when put through a venturi tube?

A

Velocity increases and then decreases

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20
Q

What is the bernoulli’s theorem described with words?

A

Mass can neither be created nor destroyed, it can only change from one form of energy to another

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21
Q

What is the bernoulli’s principle?

A

In a flow of ideal fluid, the sum of pressure and kinetic energy (per unit volume) remains constant

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22
Q

What does the bernoulli’s theorem have to do with pressure?

A

It describes that:
Static pressure + Dynamic pressure = Total pressure (Constant)

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23
Q

Describe the pressure in a venturi tube according to bernoulli’s theorem

A
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24
Q

Which types of airflow is there?

A

Laminar
Turbulent
Vortex

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25
Force = ? x ?
Pressure x area
26
What will exist if there is an asymmetry in the pressure acting on an object?
A net force
27
What is a two dimensional flow?
A flow that moves in 2 directions: Left and right Up and down
28
Describe the pressure around a cylinder
Where streamlines are close speed is faster Where flow is faster static pressure is reduced Where flow is slower static pressure is increased
29
Where can total pressure be measured on an object moving through the air?
At the stagnation point
30
Describe static pressure on a cylinder
31
What is the chord and chord line?
The chord is the 2 furthest points from leading edge to trailing edge and the line between them
32
What is the Angle of attack and what is the symbol?
33
Which 4 different aerofoil conventions is presented in the powerpoint?
34
What is camber?
Camber is the asymmetry between the two acting surfaces of an airfoil
35
What is chord ratio?
The ratio between the chord length and the aerofoil's maximum thickness
36
Describe how airflow moves across an aerofoil
Faster on top and slower underneath
37
Where is the accelerated airflow located around the wing?
Above
38
What does the differences in surface pressure at each point around the aerofoil create?
An unbalanced force
39
What is all the unbalanced forces around the aerofoil added together equal too?
The total reaction
40
Where does the total reaction originate from?
The centre of pressure (CP)
41
When a wing is lifted and the angle of attack increases where is the total reaction pointing?
Upwards and backwards
42
What is the component which is perpendicular to the free stream flow called?
Lift
43
What is the aerodynamic total reaction?
Aerodynamic total reaction = The vector for lift + The vector for drag
44
What is the stagnation line and stagnation point?
The line is the airflow towards and away from the stagnation point The stagnation point is the point where fluid's velocity is zero in the inviscid approximation
45
What does the magnitude and direction of the total reaction depend on?
The pressure distribution created around the aerofoil The overall area of the aerofoil
46
What does the pressure distribution depend on?
The speed of the flow The angle of attack Camber
47
What happens to the total reaction when airspeed doubles?
The total reaction is 4 times greater
48
Where is the total reaction pointing on a symmetrical aerofoil with zero degress angle of attack?
It's pointing backwards
49
Where is the total reaction pointing on a symmetrical aerofoil with positive degress angle of attack?
It's pointing upwards
50
Where is the total reaction pointing on a positively cambered aerofoil with zero degress angle of attack?
It's pointing upwards
51
Does the CP change if a cambered aerofoil moves upwards?
Yes, the magnitude of the total pressure increases and moves it forward
52
What does an increase in camber do?
Increase the pressure differential between the upper and lower surfaces of the aerofoil
53
Describe the 3 flows of three dimensional flow?
1st dimension - Forward and backwards 2nd dimension - Up and down 3rd dimension - Left and right (Spanwise)
54
What does spanwise flow involve?
Vortices
55
What is the direction of airflow influenced by?
The inertia of the mass of air in the flow Pressure differentials
56
Why is a vortex created on the wing and where?
It's created due to pressure differentials between upper and lower wing on the wing tip, since the lower pressure moves towards the higher
57
What does the intensity of the tip vortex depend on?
Two factors: The pressure differential - Higher equals greater vortex The amount of time the driving force is given to operate on the air mass
58
When will tip vortex intensity be reduced?
Aircraft speed increase Wing aspect ratio increase The amount of lift being produced reduces
59
What does a tip vortex produce?
Downwash Drag - Energy is used to produce a vortex
60
What does the spanwise flow produce on the trailing edge and results in drag?
Trailing edge vortices
61
Where is upwash and downwash located around the wing?
Upwash in front and downwash behind
62
What is the definition on an effective wing?
Produces the most lift with the least amount of drag
63
What do you increase in order to have more lift and produce the least amount of drag?
The aspect ratio
64
What is the disadvantages to a higher aspect ratio?
65
Where is the most and least lift generated on an eliptical wing?
Most at wing root and least at wing tip
66
Where is the most and least lift generated on an rectangular wing?
Most at wing root and least at wing tip
67
Where is the most and least lift generated on an tapered wing?
Most at midspan, then wing root and least at wing tip
68
Where is the most and least lift generated on an tapered and sweep back wing?
Most close to the wing tip less towards the wing root and least at the wing tip
69
What is washout?
Washout is a characteristic of aircraft wing design which deliberately reduces the lift distribution across the span of an aircraft's wing. The wing is designed so that the angle of incidence is greater at the wing roots and decreases across the span, becoming lowest at the wing tip
70
How is washout made?
By making a camber change so lift is gradually reduced from the root to the wing tip
71
What is wing loading?
The weight of the aeroplane divided by the wing area
72
What does a high wing loading produce?
More intense vortices

EK24 (29 decks)

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