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Heat will always attempt to flow:
It is a law of thermodynamics that heat will always flow to the cold, not the other way round.
It is a law of thermodynamics that heat will always flow to the cold, not the other way round.
Conduction is the process of heat transfer when:
A cold ground cooling the air directly above it is an example of conduction.
A cold ground cooling the air directly above it is an example of conduction.
Cool and hot water circulating in a kettle on a gas stove is an example of:
Convection is the transfer of heat via molecule movement in gases and liquids.
Convection is the transfer of heat via molecule movement in gases and liquids.
In pilot meteorology the horizontal flow of air is referred to as:
Advection is just another name for wind.
Advection is just another name for wind.
When vapour changes to water and water changes to ice, latent heat is:
To change state, any substance has to either absorb latent heat, or release it. When water changes to ice, it needs to cool down so the substance releases latent heat.
To change state, any substance has to either absorb latent heat, or release it. When water changes to ice, it needs to cool down so the substance releases latent heat.
The specific heat of water is:
It takes a lot of energy to raise the temperature of water.
It takes a lot of energy to raise the temperature of water.
The difference between height and altitude is:
If air pressure is measured at sea level anywhere on Earth this is the:
If we set the subscale on an altimeter to the current QNH we will:
The ISA pressure at sea level is:
Pressure height = ?
Pressure height indicates:
It is determined by our elevation and QNH. At a QNH of 1013, the pressure altitude will be the same as the aircraft’s actual height AMSL.
It is determined by our elevation and QNH. At a QNH of 1013, the pressure altitude will be the same as the aircraft’s actual height AMSL.
Using the information below work out pressure height.
Altitude or Elevation is: 2041
QNH: 1020
Pressure height = (1013 – QNH) x 30 + elevation
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
PH = Elevation + 30 x (1013 – QNH)
PH = 2041 + 30 x (1013 – 1020) = 1831 ft
Pressure height = (1013 – QNH) x 30 + elevation
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
PH = Elevation + 30 x (1013 – QNH)
PH = 2041 + 30 x (1013 – 1020) = 1831 ft
Using the information below work out pressure height.
Altitude or Elevation is: 3025
QNH: 1009
Pressure height = (1013 – QNH) x 30 + elevation
PH = (1013 – 1009) x 30 + 3025 = 3145 ft
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
Pressure height = (1013 – QNH) x 30 + elevation
PH = (1013 – 1009) x 30 + 3025 = 3145 ft
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
Using the information below work out pressure height.
Altitude or Elevation is: 567 ft
QNH: 1011
PH = 567 ft + 30 x (1013 – 1011) = 627 ft.
Pressure height = (1013 – QNH) x 30 + elevation
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
PH = 567 ft + 30 x (1013 – 1011) = 627 ft.
Pressure height = (1013 – QNH) x 30 + elevation
Use the calculator to learn
https://www.pilotpracticeexams.com/altitude-calculator/
The ISA Temperature at any height = ?
For every 1000 ft increase in elevation, the temperature will cool by 2 degrees in an ISA environment.
For every 1000 ft increase in elevation, the temperature will cool by 2 degrees in an ISA environment.
The ISA temp at 5000 feet =?° C
=15 – 2 x 5
=15 – 10
=5°C
=15 – 2 x 5
=15 – 10
=5°C
The ISA temp at 20,000 feet =?° C
=15 – 2 x 20
=15 – 40
=-25°C
=15 – 2 x 20
=15 – 40
=-25°C
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