aerosandbox.atmosphere._isa_atmo_functions
==========================================

.. py:module:: aerosandbox.atmosphere._isa_atmo_functions


Attributes
----------

.. autoapisummary::

   aerosandbox.atmosphere._isa_atmo_functions.gas_constant_universal
   aerosandbox.atmosphere._isa_atmo_functions.molecular_mass_air
   aerosandbox.atmosphere._isa_atmo_functions.gas_constant_air
   aerosandbox.atmosphere._isa_atmo_functions.g
   aerosandbox.atmosphere._isa_atmo_functions.isa_table
   aerosandbox.atmosphere._isa_atmo_functions.isa_base_altitude
   aerosandbox.atmosphere._isa_atmo_functions.isa_lapse_rate
   aerosandbox.atmosphere._isa_atmo_functions.isa_base_temperature
   aerosandbox.atmosphere._isa_atmo_functions.isa_pressure


Functions
---------

.. autoapisummary::

   aerosandbox.atmosphere._isa_atmo_functions.barometric_formula
   aerosandbox.atmosphere._isa_atmo_functions.pressure_isa
   aerosandbox.atmosphere._isa_atmo_functions.temperature_isa


Module Contents
---------------

.. py:data:: gas_constant_universal
   :value: 8.31432


.. py:data:: molecular_mass_air
   :value: 0.0289644


.. py:data:: gas_constant_air
   :value: 287.0530720470647


.. py:data:: g
   :value: 9.81


.. py:data:: isa_table
   :value: None


.. py:data:: isa_base_altitude

.. py:data:: isa_lapse_rate

.. py:data:: isa_base_temperature

.. py:function:: barometric_formula(P_b, T_b, L_b, h, h_b)

   The barometric pressure equation, from here: https://en.wikipedia.org/wiki/Barometric_formula
   :param P_b: Pressure at the base of the layer, in Pa
   :param T_b: Temperature at the base of the layer, in K
   :param L_b: Temperature lapse rate, in K/m
   :param h: Altitude, in m
   :param h_b:

   Returns:



.. py:data:: isa_pressure
   :value: [101325.0]


.. py:function:: pressure_isa(altitude)

   Computes the pressure at a given altitude based on the International Standard Atmosphere.

   Uses the Barometric formula, as implemented here: https://en.wikipedia.org/wiki/Barometric_formula

   :param altitude: Geopotential altitude [m]

   Returns: Pressure [Pa]



.. py:function:: temperature_isa(altitude)

   Computes the temperature at a given altitude based on the International Standard Atmosphere.

   :param altitude: Geopotential altitude [m]

   Returns: Temperature [K]