isacalc

Name	isacalc JSON
Version	1.3.3 JSON
	download
home_page	https://github.com/LukeDeWaal/ISA_Calculator
Summary	Standard International Atmosphere Calculator
upload_time	2025-02-26 14:41:52
maintainer	None
docs_url	None
author	Luke de Waal
requires_python	None
license	GNU GPLv3
keywords	isa aerospace aeronautical atmosphere
VCS
bugtrack_url
requirements	No requirements were recorded.
Travis-CI	No Travis.
coveralls test coverage	No coveralls.

            # ISACALC : A Basic ISA Calculator for Python projects

  - Accurate Atmospheric Model up to 110km
  - Accurate Calculations for Temperature, Pressure and Density
  - Option for user-defined atmospheric conditions:
    - Change the temperature gradients
    - Change the base pressure or density
    - Change physical constants such as gravity or universal gas constant for air
    - Make your custom atmosphere and save it to a JSON file to be loaded
  - Tabulate your data to save future computation time
    - Start, Stop and Step in meters
    - 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 install this package, simply `pip install isacalc`

And thats it! An simple example script:

    
```python
import isacalc as isa
    
# Default atmosphere
atmosphere = isa.Atmosphere()

print(atmosphere)

h = 50000.0

# Calculate a single time 
T, P, d, a, mu = atmosphere.calculate(h)

# Generate a table
table = atmosphere.tabulate(0, 25000, 100)
```

            

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    "description": "# ISACALC : A Basic ISA Calculator for Python projects\n\n  - Accurate Atmospheric Model up to 110km\n  - Accurate Calculations for Temperature, Pressure and Density\n  - Option for user-defined atmospheric conditions:\n    - Change the temperature gradients\n    - Change the base pressure or density\n    - Change physical constants such as gravity or universal gas constant for air\n    - Make your custom atmosphere and save it to a JSON file to be loaded\n  - Tabulate your data to save future computation time\n    - Start, Stop and Step in meters\n    - Save tabulated data in .csv or .xlsx files\n  \nWith this module, it is possible to calculate, using the 1976 standard atmosphere model, the Temperature,\nDensity and Pressure at any point in the atmosphere from 0 up to 110,000 \\[m].\n\nThis package is useful for Aerospace and Aeronautical Engineers who wish to run simulations using atmospheric data.\n\nTo install this package, simply `pip install isacalc`\n\nAnd thats it! An simple example script:\n\n    \n```python\nimport isacalc as isa\n    \n# Default atmosphere\natmosphere = isa.Atmosphere()\n\nprint(atmosphere)\n\nh = 50000.0\n\n# Calculate a single time \nT, P, d, a, mu = atmosphere.calculate(h)\n\n# Generate a table\ntable = atmosphere.tabulate(0, 25000, 100)\n```\n",
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