Atmosphere Flashcards

1
Q

Density

A

Term used to represent the number of molecules and how closely they are packed into any given volume of a substance

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2
Q

What effects air density

A

Temperature and pressure

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3
Q

Temperature effect on air density

A

As temp increases (and air isn’t contained) it’s molecules will have more KE meaning they will move further apart and so air density decreases

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4
Q

Pressure effect on air density

A

As pressure increases density also increases due to denser air having more molecules that collide with a surface and hence more pressure is generated

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5
Q

ISA

A

Is a hypothetical set of atmospheric conditions that represents an average of the conditions experienced worldwide

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6
Q

ISA pressure

A
  • sea level = 1013.2hPa
  • decreases at a rapid rate up to 5000ft (about 1hPa/30ft) and a lower rate thereafter
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7
Q

ISA Temperature

A
  • sea level = +15C
  • decreasing a uniform rate of 1.98C/1000ft up to the tropopause (which is set in the ISA as 36,090ft)
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8
Q

ISA density

A
  • sea level = 1.225 kg/m^3
  • decreases with altitude at a rapid rate initially and a lower rate thereafter
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9
Q

Altitude bands in which atmospheric pressure and density are reduced to 75%, 50%, and 25% their normal sea level values

A
  • 75% = 8,000 to 10,000ft
  • 50% = 18,000 to 22,000ft
  • 25% = 34,000 to 41,000ft
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10
Q

Density altitude

A

The altitude in the ISA that has the same air density as actual altitude, so if actual conditions differ from ISA then density altitude will be different from actual altitude by an amount depending on how much prevailing pressure and/or temp conditions differ from ISA

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11
Q

What does density altitude measure

A

Aircraft performance

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12
Q

How does humidity effect density altitude

A

As humidity increases, density decreases due to water molecules having less mass than dry air molecules so moist air is less dense than dry air therefore with a high humidity the density at a pilot’s location is equivalent to a higher altitude in the standard atmosphere. Thus the term “high density altitude.”

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13
Q

How is best aerodynamic and engine performance achieved

A
  • High pressure
  • low temp
  • dry air (low humidity)
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14
Q

Viscosity

A

Is the tendency for the molecules of a fluid to stick together and cling to any solid surface they come in contact with, it plays an important part in aerodynamics. When air moves across a perfectly flat plane surface the layer of molecules in immediate contact with the surface will be brought to a standstill because of viscosity, successive layers of air above the bottom layer will be slowed by decreasing amounts until the point is reached where the effect of viscosity is no longer felt. The layer of retarded air is called the boundary layer.

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15
Q

Boundary layer flow

A

Beginning at the outer edge of the boundary layer the velocity of the airflow is progressively decreased until it is brought to a stop at the surface. The flow within the boundary layer exists in 2 forms - laminar flow and turbulent flow

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16
Q

Laminar flow

A

The initial part of the flow over most smooth surfaces is laminar in nature which means each successive sheet of air slides smoothly over the one nearer the surface and there is a relatively uniform increase in velocity from zero at the surface to the freestream value at the outer edge.

17
Q

Laminar flow boundary layer thickness

A

2mm in depth

18
Q

Turbulent boundary layer flow

A

After progressing for a certain distance over a surface (even if that surface is flat and aligned with the airflow) the flow in the boundary layer normally becomes turbulent and the layer becomes much thicker. This turbulent boundary layer is characterized by high frequency eddies and swirls and there is considerable inter-mixing of the flows at successive levels

19
Q

Transition point

A

Is the point where the flow changes from laminar to turbulent

20
Q

Turbulent flow boundary layer thickness

A

2cm in depth