Performance#

class tuduam.performance.ISA(h, T_offset=0)[source]#

Bases: object

Calculates the atmospheric parameters at a specified altitude h (in meters). An offset in sea level temperature can be specified to allow for variations.

Note: Since our aircraft probably doesn’t fly too high, this is only valid in the troposphere

density()[source]#

pressure()[source]#

soundspeed()[source]#

temperature()[source]#

viscosity_dyn()[source]#