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  ThermoFluidCalc — Standalone Fortran Execution Guide
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Calculator : Airfoil Vortex Panel & Induced Drag
Category   : Cfd

Files Included:
  - airfoil_panel_method_vortex.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 airfoil_panel_method_vortex.f90 -o airfoil_panel_method_vortex

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

  airfoil_panel_method_vortex < input.txt

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3. Input Parameter Sequence
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Airfoil Chord [mm]\nWing Aspect Ratio AR\nOswald Efficiency Factor e\nAngle of Attack [deg]\nNACA Max Camber [% chord]\nNACA Camber Position [tenths]\nNACA Max Thickness [% chord]

Website : https://thermofluidcalc.com
