Chapter 1 Flashcards

(42 cards)

1
Q

What height is the tropopause and troposphere?

A

Between 7.5km and 16.5km

Usually 11km

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2
Q

Whats ISA?

A

International Standard Atmosphere

A standard atmosphere defined in the troposphere and stratosphere for comparison of aircraft performance, calibration of altimeters, and other.

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3
Q

Whats the ISA for pressure at sea level?

A

1013.2 mb

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4
Q

Whats the ISA for density at sea level?

A

1.226 kg/m ^3

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5
Q

Whats the ISA for temperature at sea level?

A

15 degrees celcius

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6
Q

Whats maximum camber

A

Maximum distance between the mean camber line and the chord line

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7
Q

Whats an aerofoil?

A

Any surface which when inclined to an airflow will provide a lifting surface

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8
Q

Whats chord ratio?

A

The ratio of the maximum thickness to the chord length

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9
Q

Whats the Angle of Attack?

A

The Angle between chord line and relative airflow

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10
Q

Whats angle of incidence? (AOI)

A

The angle between the chord line and the fixed aircraft datum line?

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11
Q

Whats the span?

A

The distance from wing tip to wing tip

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12
Q

Whats the aspect ratio? (AR)

A

Ratio of wing span to chord

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13
Q

What are the temperature changes for an increase in altitude? M & ft

A

6.5 degrees Celsius per km

2 degrees Celsius per 1000ft

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14
Q

Whats Static stability?

A

An objects immediate response to a disturbance

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15
Q

Whats dynamic stability?

A

Response over time following a disturbance

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16
Q

Whats unstable (negative stability)?

A

Object that never returns to original place after disturbance

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17
Q

Whats stable (positive stability)?

A

Returns back to original position

18
Q

Whats Neutrally stable?

A

Neither returns to or continues away from original position

19
Q

What axis is a rolling motion?

20
Q

What axis is pitch?

21
Q

What axis is yawing?

22
Q

Effects of ice forming on an aircraft?

A

Drag
Weight (overnight)
CoG displaced
Vibration
Stiff controls
Vision impaired
Undercarriage locked
Engine & intake components damaged by ice

23
Q

At what temp can snow form on aircraft?

A

When isotherm is below 0 degree C

24
Q

Where does ice form the quickest?

A

Objects with a thin cross section
- pitot
- rotor blades
- leading edges

25
Whats hoar frost?
Light deposits that form on aircraft skin at 0 degrees C or lower when on a rapid descent or after being parked outside on a clear winter night. Restricts visibility.
26
Whats the tropopause?
Pause section where temperature stabilises in between the troposphere & stratosphere
27
Whats the stratosphere?
Temperature increases section due to ozone layer
28
Whats viscosity?
Fluids (liquid or gas) resistance to internal friction
29
Whats the formula for pressure and density?
P = ma D = m/v
30
Whats the boundary layer?
Airflow slowed due to viscosity and friction close to the aerofoil surface 0.1-0.2mm thick 5mm - no lift
31
Whats laminar flow?
Neat orderly flow over an object
32
What are the 3 types of aerofoil shape?
High lift - curved shape (more drag) High speed - sharp leading and trailing edge General purpose
33
Whats the stalling angle?
15-16 degrees
34
Whats the stalling speed?
Slowest speed it can be flown before not enough lift is produced
35
Whats the total reaction?
Resultant force of lift and drag
36
What factors affect lift?
Density Velocity Shape Surface area AoA Surface finish Dynamic pressure
37
What are the 4 leading edge augmentation devices?
Slot - permanent fit allows airflow from lower to upper camber makes turbulent flow laminar Slat - pitot or automatically operated (not permanent) Kreuger flap (leading edge) Droop nose
38
What are the 3 trailing edge devices?
Flaps - plain - split - fowler (best)
39
What two groups make up total drag?
Lift dependant Zero lift (drag)/ parasite drag
40
What component parts make up lift dependant drag?
Form drag Skin friction drag Induced/ vortex drag
41
Zero lift drag Parasite drag
Form drag Skin friction drag Interference drag
42
Whats TP & SP in regards to boundary layer?
TP - transition point where the layer goes from laminar to turbulent SP - when the air becomes too turbulent to continue following the profile of the aerofoil After separation there is no lift