jbrillon / compressible-Blasius-solver

Robust solver for the compressible Blasius equations for laminar, high-speed flow, boundary layers over a flat plate.
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aerodynamics blasius-equation boundary-layer compressible-flow

Date written: December 2018

As part of final project for ME 614 (Computational Fluid Dynamics) at Purdue University taught by Professor Scalo of the Mechanical Engineering department.

Compressible Blasius Equations Solver

Solves the compressible Blausius equations for laminar, high-speed flow, boundary layers over a flat plate with either isothermal (Dirichlet) or adiabatic (Neumann) boundary conditions. Computes the resulting near-wall velocity and temperature profiles. Results are shown below. For more details, refer to the report by clicking here.