Barometric formula

For broader coverage of this topic, see Vertical pressure variation.

The barometric formula is a formula used to model how the air pressure (or air density) changes with altitude.

Model equations

See also: Atmospheric pressure

Pressure as a function of the height above the sea level

The U.S. Standard Atmosphere gives two equations for computing pressure as a function of height, valid from sea level to 86 km altitude. The first equation is applicable to the atmospheric layers in which the temperature is assumed to vary with altitude at a non null temperature gradient of ${\displaystyle L_{M,b}}$: $${\displaystyle P=P_{b}\cdot \left[{\frac {T_{M,b}}{T_{M,b}+L_{M,b}\cdot \left(H-H_{b}\right)}}\right]^{\frac {g_{0}'\cdot M_{0}}{R^{*}\cdot L_{M,b}}}}$$ .^[1]: 12

The second equation is applicable to the atmospheric layers in which the temperature is assumed not to vary with altitude (zero temperature gradient): $${\displaystyle P=P_{b}\cdot \exp \left[{\frac {-g_{0}'\cdot M_{0}\left(H-H_{b}\right)}{R^{*}\cdot T_{M,b}}}\right]}$$ ,^[1]: 12 where:

• ${\displaystyle P_{b}}$ = reference pressure
• ${\displaystyle T_{M,b}}$ = reference temperature (K)
• ${\displaystyle L_{M,b}}$ = temperature gradient (K/m), e.g. -6.5 K/km at sea level. This is the lapse rate with the opposite sign convention.
• ${\displaystyle H}$ = geopotential height at which pressure is calculated (m)
• ${\displaystyle H_{b}}$ = geopotential height of reference level b (meters; e.g., H_b = 11 000 m)
• ${\displaystyle R^{*}}$ = universal gas constant: 8.31432 N·m/(kmol·K)^[1]: 3
• ${\displaystyle g_{0}'}$ = The gravitational acceleration in units of geopotential height, 9.80665 m/s^2[1]: 3
• ${\displaystyle M_{0}}$ = mean molecular weight of air at sea level: 28.9644 kg/kmol^[1]: 9

Or converted to imperial units:^[2]

• ${\displaystyle P_{b}}$ = reference pressure
• ${\displaystyle T_{M,b}}$ = reference temperature (K)
• ${\displaystyle L_{M,b}}$ = temperature gradient (K/ft)
• ${\displaystyle H}$ = height at which pressure is calculated (ft)
• ${\displaystyle H_{b}}$ = height of reference level b (feet; e.g., H_b = 36,089 ft)
• ${\displaystyle R^{*}}$ = universal gas constant; using feet, kelvins, and (SI) moles: 8.9494596×10⁴ lb·ft²/(lb-mol·K·s²)
• ${\displaystyle g_{0}}$ = gravitational acceleration: 32.17405 ft/s²
• ${\displaystyle M}$ = molar mass of Earth's air: 28.9644 lb/lb-mol

The value of subscript b ranges from 0 to 6 in accordance with each of seven successive layers of the atmosphere shown in the table below. In these equations, g₀, M and R^* are each single-valued constants, while P, L, T, and H are multivalued constants in accordance with the table below. The values used for M, g₀, and R^* are in accordance with the U.S. Standard Atmosphere, 1976, and the value for R^* in particular does not agree with standard values for this constant.^[1]: 3 The reference value for P_b for b = 0 is the defined sea level value, P₀ = 101 325 Pa or 29.92126 inHg. Values of P_b of b = 1 through b = 6 are obtained from the application of the appropriate member of the pair equations 1 and 2 for the case when H = H_b+1.^[1]: 12

Subscript b	Geopotential height above MSL (H)[1]: 3		Static pressure		Standard temperature (K)	Temperature gradient[1]: 3		Exponent g0 M / R L
	(km)	(ft)	(Pa)	(inHg)		(K/km)	(K/ft)
0	0	0	101 325	29.9213	288.15	-6.5	-0.0019812	-5.25588
1	11	36 089	22 632.1	6.68324	216.65	0.0	0.0	—
2	20	65 617	5 474.89	1.616734	216.65	1.0	0.0003048	34.1626
3	32	104 987	868.019	0.256326	228.65	2.8	0.00085344	12.2009
4	47	154 199	110.9063	0.0327506	270.65	0.0	0.0	—
5	51	167 323	66.9389	0.0197670	270.65	-2.8	-0.00085344	-12.2009
6	71	232 940	3.95642	0.00116833	214.65	-2	-0.0006096	-17.0813

Density can be calculated from pressure and temperature using

${\displaystyle \rho ={\frac {P\cdot M_{0}}{R^{*}\cdot T_{M}}}={\frac {P\cdot M}{R^{*}\cdot T}}}$ ,^[1]: 15 where

• ${\displaystyle M_{0}}$ is the molecular weight at sea level
• ${\displaystyle M}$ is the mean molecular weight at the altitude of interest
• ${\displaystyle T}$ is the temperature at the altitude of interest
• ${\displaystyle T_{M}=T\cdot {\frac {M_{0}}{M}}}$ is the molecular-scale temperature.^[1]: 9

The atmosphere is assumed to be fully mixed up to about 80 km, so ${\displaystyle M=M_{0}}$ within the region of validity of the equations presented here.^[1]: 9

Alternatively, density equations can be derived in the same form as those for pressure, using reference densities instead of reference pressures.^{[citation needed]}

This model, with its simple linearly segmented temperature profile, does not closely agree with the physically observed atmosphere at altitudes below 20 km. From 51 km to 81 km it is closer to observed conditions.^[1]: 1

Derivation

The barometric formula can be derived using the ideal gas law: $${\displaystyle P={\frac {\rho }{M}}{R^{*}}T}$$

Assuming that all pressure is hydrostatic: $${\displaystyle dP=-\rho g\,dz}$$ and dividing this equation by ${\displaystyle P}$ we get: $${\displaystyle {\frac {dP}{P}}=-{\frac {Mg\,dz}{R^{*}T}}}$$

Integrating this expression from the surface to the altitude z we get: $${\displaystyle P=P_{0}e^{-\int _{0}^{z}{Mgdz/R^{*}T}}}$$

Assuming linear temperature change ${\displaystyle T=T_{0}-Lz}$ and constant molar mass and gravitational acceleration, we get the first barometric formula: $${\displaystyle P=P_{0}\cdot \left[{\frac {T}{T_{0}}}\right]^{\textstyle {\frac {Mg}{R^{*}L}}}}$$

Instead, assuming constant temperature, integrating gives the second barometric formula: $${\displaystyle P=P_{0}e^{-Mgz/R^{*}T}}$$

In this formulation, R^* is the gas constant, and the term R^*T/Mg gives the scale height (approximately equal to 8.4 km for the troposphere).

(For exact results, it should be remembered that atmospheres containing water do not behave as an ideal gas. See real gas or perfect gas or gas for further understanding.)

See also

• Hypsometric equation
• NRLMSISE-00