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  ThermoFluidCalc — Offline Fortran Execution Guide
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Calculator : Aerodynamic Lift & Drag Solver
Category   : Cfd

Files Included:
  - lift_drag.f90 (Fortran Source Code)
  - input.txt (Pre-configured Sample Input)

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1. How to Compile
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Make sure you have a Fortran compiler installed (like gfortran).
Run the following compilation command in your terminal:

  gfortran -O3 lift_drag.f90 -o lift_drag

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

  lift_drag < input.txt

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3. Input File Details
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The input file 'input.txt' contains sequential parameters separated by
newlines. Here is the structure of the included 'input.txt':

  Line 1 ((kg/mÂ³)\nV (m/s)\nS wing area (mÂ²)\nb wingspan (m)\ne Oswald eff.\nCD0\nCL (per rad)\n0 (Â°)\n0 (Â°)): 1.225
  Line 2 (Parameter 2): 60.0
  Line 3 (Parameter 3): 16.2
  Line 4 (Parameter 4): 11.0
  Line 5 (Parameter 5): 0.8
  Line 6 (Parameter 6): 0.034
  Line 7 (Parameter 7): 5.7
  Line 8 (Parameter 8): 5.0
  Line 9 (Parameter 9): -2.0

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ThermoFluidCalc — https://thermofluidcalc.com
