Meteorology Flashcards
(441 cards)
Constituents of gas in atmosphere
Nitrogen: 78%
Oxygen: 21%
Argon: <1%
CO2, ozone (O3) etc.
Percentage of water vapour in atmosphere
0.001% to 4%
Averages less than 1%
NOTE: This isn’t included in the usual breakdown of atmosphere which is based on DRY air
Temperature changes in stratosphere
Constant up to 20km
Increases up to -15C at 50km
Decreases from 51km again (stratopause)
Reason for increase in temperature with altitude in stratosphere
O2 breaks down into 2 O molecules by absorbing UV light (<240nm wavelength), which is exothermic.
Single O’s join with other O2 to form ozone (O3).
O3 absorbs UV light (<290nm wavelength) to breakdown into O2 and O, again exothermic.
Tropopause definition
Point where temperature stops falling with altitude increase (taken as rate of fall going below 0.61C per 1000ft - 2C per 1km)
What factor impacts tropopause height and temperature?
Temperature depends on height, the higher it is the more temperature is lost before reaching it.
Height is determined by surface temperature, high surface temp (equator) leads to higher altitude (thus high surface temp leads to low tropopause temp).
Typical tropopause heights and temperatures
53,000ft (16km) at equator, -75C.
36,000ft (11km) at mid-lat, -56C.
26,000ft (8km) at poles, -45C.
Tropopause heights summer & winter
- Latitudes 30, 50, 70
Summer Winter
30deg: 16km 16km
50deg: 12km 9km
70deg: 9km 8km
Mesosphere, thermosphere and exosphere altitudes
Mesosphere: 50km to 85km
Thermosphere: 85km to 600km
Exosphere: 600km to 10,000km
Mesosphere and Thermosphere features
Mesosphere: Meteors are burned up by the thickness of atmosphere here
Thermosphere: Absorption of high energy UV and X-rays leads to increasing temperature with altitude around -120C at base to 2000C at top.
ISA
- MSL temp, pressure, density
- lapse rates
- MSL temp 15C
- MSL pressure 1013.25 hPa
- MSL density 1.225kg / m3
- Lapse rate 1.98C / 1000ft to 36k
- Constant temp up to 20km
- Temp increase 1C / 1km to 32km
Pressure levels by altitude
30000’ 300
18000’ 500
10000’ 700
Altitude of:
- 50% of MSL pressure
- 50% of MSL density
- 50% of weight of atmosphere below
18,000ft: 50% pressure
20,000ft: Half weight of atmosphere
22,000ft: 50% density
Altitude of 25% MSL density
40,000ft
Barograph
Aneroid type pressure capsule connected to rotating drum which draws a line over time as pressure increases and reduces
Equation for (H), height change in feet per hPa
H = (96 x T) / P
T = Temperature in Kelvin
P = Pressure in hPa
Height change per hPa under ISA at:
MSL, 20000’, 40000’
MSL = 30 feet per hPa
20000’ = 50 feet per hPa
40000’ = 100 feet per hPa
Diurnal pressure variation
1hPa typically but up to 3hPa in tropics.
Needs to be considered as part of assessment of pressure changes over time.
QFE (Field Elevation)
Pressure setting to give zero elevation at HIGHEST point on airfield.
If touchdown point is significantly lower you may be given a touchdown QFE.
QFF
Similar to QNH (nautical height) but converts QFE to MSL using actual temperatures rather than ISA temperatures to establish true MSL pressure at a location which is relevant to meteorological charts.
Note - QNH gives correct airfield elevation when at the airfield.
QFF vs QNH when temp is higher than ISA and airfield above sea level
If warm and > sea level:
QNH > QFF
Flips if cold, both flip if below sea level.
QNE
NOT a pressure setting. This is the height on altimeter at touchdown point if standard pressure setting (1013) is set.
Used for high elevation airfields where QFE is too low to set in altimeter.
Risk of ground collision when heading to high or low pressure
Altimeter will over-read if heading into low pressure risking ground collision.
Think about what would happen if you adjusted to the correct pressure setting (turn down to the lower pressure setting, indicated altitude would fall).
Density altitude
- description
- calc
The altitude at which observed air density would be found in an ISA standard atmosphere.
Or, pressure altitude adjusted for ISA temperature difference (@120ft per C)