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CFD CODE
During my Masters Degree at Embry-Riddle, I built and verified a 2-D Euler solver in MATLAB by obtaining steady-state solutions for the inviscid flow over an 4% bump at subsonic, transonic, and supersonic speeds using a first-order upwind Van Leer flux scheme and explicit time advancement.
CFD Code: About
The grid used in the project consisted in 100 and 40 cells in the X and Y direction respectively, with a total of 4,000 cells.
CFD Code: About
Residual graphs were generated in order to verify that the simulation was converging.
CFD Code: About
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