Standard International Atmosphere Calculator
Project description
ISA Calculator
==> Basic ISA Calculator for Python projects
- Contents:
Atmospheric Model up to 110km
Accurate Calculations for Temperature, Pressure and Density
Custom defined atmospheric conditions
Tabulate your data to save future computation time
Save tabulated data in .csv or .xlsx files
With this module, it is possible to calculate, using the 1976 standard atmosphere model, the Temperature, Density and Pressure at any point in the atmosphere from 0 up to 110,000 [m].
This package is useful for Aerospace and Aeronautical Engineers who wish to run simulations using atmospheric data.
To use this package, follow these steps:
Install isacalc
Import isacalc as isa
Define the Atmosphere Model: isa.get_atmosphere()
Calculate all parameters at a cetain height: isa.calculate_at_h(h, atmosphere_model)
- It calculates, at the defined height:
Temperature
Pressure
Density
Speed of sound
Dynamic Viscosity
And thats it! An example Script:
import isacalc as isa
atmosphere = isa.get_atmosphere()
h = 50000.0
T, P, d, a, mu = isa.calculate_at_h(h, atmosphere)
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