Calculates atmospheric pressure as a function of elevation, by default assuming standard atmosphere (101325 Pa at sea level)
calc_patm(elv, patm0 = 101325)
A numeric value for \(p\)
The elevation-dependence of atmospheric pressure is computed by
assuming a linear decrease in temperature with elevation and a mean
adiabatic lapse rate (Berberan-Santos et al., 1997):
$$
p(z) = p0 ( 1 - Lz / TK0) ^ ( g M / (RL) )
$$
where \(z\) is the elevation above mean sea level (m, argument elv
),
\(g\) is the gravity constant (9.80665 m s-2), \(p0\) is the atmospheric
pressure at 0 m a.s.l. (argument patm0
, defaults to 101325 Pa),
\(L\) is the mean adiabatic lapse rate (0.0065 K m-2),
\(M\) is the molecular weight for dry air (0.028963 kg mol-1),
\(R\) is the universal gas constant (8.3145 J mol-1 K-1), and \(TK0\)
is the standard temperature (298.15 K, corresponds to 25 deg C).
Allen, R. G., Pereira, L. S., Raes, D., Smith, M.: FAO Irrigation and Drainage Paper No. 56, Food and Agriculture Organization of the United Nations, 1998