Chapter 1.1 - Aerodynamics Review Flashcards

(58 cards)

1
Q

Name four types of Aerofoil?

A
  • Wings.
  • Horizontal Stabilisers.
  • Vertical Stabilisers.
  • Propeller Blade.
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2
Q

Define Chord Line?

A

Imaginary straight line from the leading to trailing edge of a wing.

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3
Q

Define Wingspan?

A

Distance from wingtip to wingtip.

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4
Q

Name another word to describe the curvature of a wing?

A

Camber.

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5
Q

An Aerofoil with zero Camber is said to be what?

A

Symmetrical.

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6
Q

The Relative Airflow acts in what direction of the Flight Path?

A

Opposite.

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7
Q

Define Angle of Attack?

A

The angle between Relative Airflow and Chord Line.

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8
Q

Relative Airflow and Angle of Attack are related to what?

A

Flight Path.

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9
Q

Lift acts in what direction to the Relative Airflow?

A

Perpendicular.

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10
Q

Drag acts in what direction to the Relative Airflow?

A

Same Direction/Parallel.

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11
Q

Name two types of Wing Drag?

A
  • Induced.

- Parasite.

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12
Q

How is Induced Drag formed?

A

Through the production of Lift.

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13
Q

Name two types of Parasite Drag?

A
  • Form Drag.

- Skin Friction.

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14
Q

Name the point on the Chord Line where Total Reaction acts through?

A

Centre of Pressure.

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15
Q

As Angle of Attack is increased, in which direction does the Centre of Pressure move?

A

Forward.

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16
Q

The maximum lift/drag ratio is at an Angle of Attack of how many degrees?

A

4°.

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17
Q

What is the Stalling Angle?

A

16°.

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18
Q

True or False. The Aerofoil Shape has a major effect in the generation of Lift?

A

True.

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19
Q

The (greater/lower) the Camber, the more lift is produced?

A

Greater.

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20
Q

Name a control surface which a Pilot can use to increase the Camber of a wing?

A

Flaps.

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21
Q

Define Thickness of an Aerofoil?

A

The greatest distance between the upper and lower surfaces of an Aerofoil.

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22
Q

The Angle of Attack for maximum Lift is called what?

A

Stalling Angle.

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23
Q

Define Angle of Incidence?

A

Angle between Chord Line and the Longitudinal Axis.

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24
Q

What’s the main difference between Angle of Incidence and Angle of Attack?

A

Angle of Attack can be altered by the Pilot. Angle of Incidence is fixed by design of the Aircraft.

25
The value of Dynamic Pressure depends on what two factors?
- Speed of Air-Flow. | - Density of the Air.
26
True or False. Lift also depends on Airspeed and Density?
True.
27
For Lift to remain constant, if Angle of Attack is increased, what must happen to the Airspeed?
Decreased.
28
For Lift to remain constant, at low IAS, what must happen to the Angle of Attack?
Increased.
29
What is the Plan Area of a Wing?
Wingspan x Chord.
30
Name five factors which affect Lift Production?
- Aerofoil/Wing Shape. - Wing Area. - Air Density. - Airspeed. - Angle of Attack.
31
What is Total Drag?
Sum of Induced and Parasite Drag.
32
How is Induced Drag created?
From Wingtip Vortices through the production of Lift.
33
True or False. Induced Drag is produced by the Aircraft (2)?
False. Only the Wings when Lift is being generated.
34
What configuration is an Aircraft in to produce High Induced Drag?
High Angles of Attack and Low Airspeeds.
35
True or False. The closer to the Stalling Angle, the higher the Induced Drag?
True.
36
Define Aspect Ratio?
Ratio of the Wing Span and Wing Chord.
37
The amount of Skin Friction depends on what factors (4)?
- Total Surface Area of the Aircraft. - Boundary Layer. - Airspeed. - Density.
38
What determines the size of wake being created behind an Aircraft?
Degree of Streamlining.
39
How can Interference Drag be reduced (3)?
- Wing Fairings. - Wing Fillets. - Streamlining.
40
Parasite Drag (increases/decreases) with increased IAS?
Increases.
41
Induced Drag (increases/decreases) with increased IAS?
Decreases.
42
At (low/high) angles of attack, Induced Drag is highest?
High.
43
At (low/high) angles of attack, Parasite Drag is highest?
Low.
44
True or False. The Minimum Drag Speed is also the speed for Maximum Lift/Drag ratio?
True.
45
True of False. The Maximum Lift/Drag ratio is the same speed for Best Glider Performance?
True.
46
True or False. The speed for Maximum Lift/Drag ratio is the same as Normal Cruise.
False. It’s less.
47
Name three symptoms of an approaching Stall?
- Control Buffet/Shaking. - Sloppy Control Response. - Stall Warning Devices.
48
The Stall Speed depends on what two factors?
- Load Factor. | - Gross Weight.
49
What percentage is used to identify the new Stall Speed at a bank angle of 30°?
+10%.
50
What percentage is used to identify the new Stall Speed at a bank angle of 45°?
+20%.
51
What percentage is used to identify the new Stall Speed at a bank angle of 60°?
+40%.
52
Name three factors that increase the Stall Speed?
- Turbulence. - Load Factor. - Frost and Ice.
53
Name two factors that decrease the Stall Speed?
- Increase in Engine Power (RPM). | - Flaps are lowered.
54
How is a Spin caused?
By an asymmetric Stall (one wing stalls before the other).
55
The Airspeed in a Spin is what?
Low and Constant.
56
How is a Spiral Dive caused?
The wings remain unstalled, but the Airspeed, Rate of Turn and Descent increases,
57
The Airspeed in a Spiral Dive is what?
High and Increasing.
58
How does a Pilot recover from a Spiral Dive (3)?
- Reduce Acceleration by closing the Throttle. - Stop the Roll with Ailerons. - Pull out of Drive.