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  ThermoFluidCalc — Standalone Fortran Execution Guide
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Calculator : Rocket Nozzle Design (De Laval)
Category   : Fluid

Files Included:
  - rocket_nozzle.f90 (Fortran 90/2008 Source Code)
  - input.txt (Pre-configured Sample Input)

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1. How to Compile
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Make sure you have GNU Fortran (gfortran) or Intel Fortran (ifort) installed.
Run the following compilation command in your terminal:

  gfortran -O3 rocket_nozzle.f90 -o rocket_nozzle

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2. How to Execute
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Run the compiled binary and pipe the input.txt file into stdin:

  rocket_nozzle < input.txt

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3. Input Parameter Sequence
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Chamber pressure Pc\nChamber temperature Tc\nSpecific heat ratio Î³\nMolar mass [kg/kmol]\nExit pressure Pe\nAmbient pressure Pa\nThroat diameter Dt

Website : https://thermofluidcalc.com
