Properties of air Flashcards

1
Q

Why is the proportion of each of the constituent gases of air not important aerodynamically

A

All have equal value for the way in which they add to the mass of air

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2
Q

What is oxygen needed for

A

To sustain the power produced by the engine and the life of the pilot

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3
Q

How is density calculated

A

The total mass contained in a given volume

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4
Q

Why is density important

A

Determines how well an aircraft and its engine can perform, as an aircraft climbs the density of air around it decreases and the wings of aircraft become less able to generate lift, at the same time the power output of the engine reduces

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5
Q

What is the easiest way to calculate density

A

By using pressure and temperature

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6
Q

What is pressure

A

The total force acting on a given area

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7
Q

Units of pressure

A

n/m-2 or Pa

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8
Q

What is atmospheric pressure usually measured in

A

hPa

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9
Q

Relationship between pressure and density

A

The higher the density the higher the pressure

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10
Q

What is tempreture

A

A measure of how much energy the molecules of a substance have or how fast they vibrate

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11
Q

In masses of air with the same temperature, that with the ______ pressure has the highest density

A

Highest

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12
Q

How far does the atmosphere extend from the earths surface

A

500 miles

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13
Q

Why is the air nearest the earths surface the densest

A

The weight of the air in the outermost reaches bears down on the air nearer the surface and compresses it

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14
Q

What happens to pressure, temperature, and density in the troposphere

A

They all decrease with altitude

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15
Q

What does ISA standard for

A

International standard atmosphere

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16
Q

What is the ISA

A

A hypothetical set of atmospheric conditions, which represents an average of the conditions experienced worldwide

17
Q

ISA initial sea level pressure

A

1013.2 hPa

18
Q

ISA pressure decrease rate

A

Pressure decreasing with altitude at a rapid rate initially around 1 hPa every 30ft to 5,000 ft and at a lower rate thereafter

19
Q

ISA initial sea-level temperature

A

+15C

20
Q

ISA temperature decreasing rate

A

Decreasing at a uniform rate of 1.98C/1000ft up to 36,090 ft

21
Q

ISA initial sea-level density

A

1.225kg/m3

22
Q

ISA density decreasing rate

A

Decreasing with altitude at a rapid rate initially and a lower rate thereafter

23
Q

What will a high temperature indicate

A

Low density and poorer performance

24
Q

What will a low temperature indicate

A

High density and better performance

25
Q

What will a high pressure indicate

A

High density and better performance

26
Q

What will a low pressure indicate

A

Low density and poorer performance

27
Q

What is density altitude

A

The altitude in the ISA which has the same density as the actual altitude you are trying to measure

28
Q

How is the density altitude worked out

A

Enter the temperature and pressure into the aircraft’s performance chart, use the navigation computer to work it out or do a manual calculation

29
Q

The hypothetical ISA is based on ___ air

A

Dry

30
Q

Range of average humidity in the air

A

20-80%

31
Q

How does humidity affect the density

A

Moist air is less dense than dry air as water molecules have less mass than the molecules of dry air it has replaced

32
Q

What is viscosity

A

The tendency for molecules of fluid to stick together and cling to any solid surface they come in contact with

33
Q

In masses of air with the same pressure, that with the ______ temperature has the highest density

A

Lowest