Automated Flow Characterisation for Low Temperature Reactions Kinetics
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Updated
Jun 19, 2024 - HTML
Automated Flow Characterisation for Low Temperature Reactions Kinetics
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
A compressible, flat-plate, laminar boundary layer solver in Julia! This routine computes the velocity and temperature profiles with variable viscosity and thermal conductivity. The numerical results are validated against wind-tunnel measurements.
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