STANDARD ATMOSPHERE (TROPOSPHERE)
Standard Atmosphere (Troposphere)
Standard Atmosphere within the troposphere (below 11.0 km)
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The pressure at zero altitude is po = 1013.250 mb.
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The temperature at zero pressure-altitude is To = 288.15K
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The lapse rate of temperature
is constant.
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The standard atmosphere satisfies ideal gas law
where
is the density of the air and Rd is
the gas constant for dry air (= 287.04 J kg-1 K-1).
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The standard atmosphere is hydrostatic
where g is the acceleration due to gravity and is constant (=
9.80665 m s-2) if z is measured in geopotential height.
Pressure-Height Relationship in Standard Atmosphere
Combining the hydrostatic equation and the ideal gas law,
pressure-height (p, z) relationship can be found by integrating the
above equation :
Density-Height Relationship in Standard Atmosphere
Starting fromt he pressure-height relationship above and replacing pressure
with density using the ideal gas law, we get :
Pressure altitude measures the altitude which corresponds to a given value
of atmospheric pressure according to the standard atmosphere.
Input :pressure reading
Output : the height will be the pressure altitude
Density altitude measures the altitude which corresponds to a given value
of atmospheric density according to the standard atmosphere. Water
vapor is neglected here.
Input :density reading (calculated from pressure and temperature
using ideal gas law, see http://hurri.kean.edu/~yoh/calculations/idealgas
)
Output : the height will be the density altitude
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The calculations is performed between -500 meter to 11000 meter of the
troposphere.
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All quantities must be in SI units. For help, try the Unit Conversion
Calculators at :
http://hurri.kean.edu/~yoh/calculations/units
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Input One of the following and hit ENTER
Report any errors in the calculators
or send any suggestions to
yoh@hurri.kean.edu
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