Pressure in atmosphere

From wikiluntti

Introduction

ISO2533:1975

The case in Toposhere (<10 km).

  • Lapse rate +6.5 °C/km
  • Base temp 19.0 °C
  • Base atmospheric pressure 108,900 Pa equals 1.075 atm
  • Base atmospheric density 1.2985 kg/m3

International Standard Atmosphere

https://en.wikipedia.org/wiki/International_Standard_Atmosphere

Consider the function in GY91's BMP280-3.3, eg at https://startingelectronics.org/tutorials/arduino/modules/pressure-sensor/

Earth's atmosphere's changes in

  • Pressure
  • Temperature
  • Density
  • Viscosity or

Hydrostatic balance The ideal gas law

Reference atmospheric model

How the ideal gas properties change (mainly) as a function of altitude (etc).

Static atmospheric model

and (see above).

Standard atmosphere

Isothermal-barotropic approximation and scale height

Temperature and molecular weight are constant: density and pressure are exponential functions of altitude.

The US standard atmosphere

More realistic temperature function, consisting of eight data points connected by straight lines, which is---of course---an approximation.

https://en.wikipedia.org/wiki/U.S._Standard_Atmosphere

NRLMSISE-00

Is an empirical, global reference atmospheric model of the Earth from ground to space.

NASA Global Reference Atmospheric Models GRAM

Barometric formula

https://en.wikipedia.org/wiki/Barometric_formula

Models how the pressure of the air changes with altitude with linear temperature change.

Ideal gas law , where pressure is a function of , thus and the hydrostatic assumption are needed to derive this.

Assume and which gives and we have

Actually, both and are dependent on altitude . Thus, we will assume linear dependency on temperature , and we have

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle \begin{align} \frac {dp}{dh}&=- g \frac{pM}{R(T_0 - Lh)} \\ \frac {dp}{p}&=- g \frac{M}{R(T_0 - Lh)} dh \\ \ln p &= \frac{gM}{RL} \ln(T_0 - hL) + C \\ p &= p_0 \left( T_0 - hL \right)^{\frac{gM}{RL}} \end{align} }

and this gives for altitude Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle h}

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle h = \frac{T_0 - \left( \frac{p}{p_0}\right)^{\frac{LR}{gM} }}{L} }



Simplified model from Weather.gov

https://www.weather.gov/media/epz/wxcalc/pressureAltitude.pdf

Failed to parse (SVG (MathML can be enabled via browser plugin): Invalid response ("Math extension cannot connect to Restbase.") from server "https://wikimedia.org/api/rest_v1/":): {\displaystyle h = 44307.70\left( 1 - \left( \frac{p}{1013.25} \right)^{0.190284} \right) }