stdatm.speed_parameters module
Functions for computation of atmosphere speed parameters.
- stdatm.speed_parameters.compute_tas_from_mach(mach, speed_of_sound)[source]
- Parameters
mach – no unit
speed_of_sound – in m/s
- Returns
true airspeed in m/s
- stdatm.speed_parameters.compute_tas_from_eas(equivalent_airspeed, density)[source]
- Parameters
equivalent_airspeed – in m/s
density – in kg/m**3
- Returns
true airspeed in m/s
- stdatm.speed_parameters.compute_tas_from_unit_re(unitary_reynolds, kinematic_viscosity)[source]
- Parameters
unitary_reynolds – in 1/m
kinematic_viscosity – in m**2/s
- Returns
true airspeed in m/s
- stdatm.speed_parameters.compute_tas_from_pdyn(dynamic_pressure, density)[source]
- Parameters
dynamic_pressure – in Pa
density – in kg/m**3
- Returns
true airspeed in m/s
- stdatm.speed_parameters.compute_mach(true_airspeed, speed_of_sound)[source]
- Parameters
true_airspeed – in m/s
speed_of_sound – in m/s
- Returns
Mach number (no unit)
- stdatm.speed_parameters.compute_equivalent_airspeed(true_airspeed, density)[source]
- Parameters
true_airspeed – in m/s
density – in kg/m**3
- Returns
equivalent airspeed in m/s
- stdatm.speed_parameters.compute_unitary_reynolds(true_airspeed, kinematic_viscosity)[source]
- Parameters
true_airspeed – in m/s
kinematic_viscosity – in m**2/s
- Returns
unitary_reynolds in 1/m
- stdatm.speed_parameters.compute_dynamic_pressure(true_airspeed, density)[source]
- Parameters
true_airspeed – in m/s
density – in kg/m**3
- Returns
incompressible dynamic pressure in Pa