Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
To simulate quasi one dimensional compressible Euler equations. This codes solves nozzle flows
Repository for Basilisk C and Python script for Coaxial Flow Simulation for my 3rd Year Individual Project.
analytical solver for laval nozzle flow with sonic shock
CFD investigation of compressible flow through a 2D axisymmetric converging-diverging nozzle using ANSYS Fluent. Includes geometry development, mesh generation, solver setup, flow-field analysis, centerline data extraction, and engineering interpretation of near-choking nozzle behavior.
Browser-based compressible-Euler lab: 1D shock tube, quasi-1D nozzle, and 2D Cartesian flows with HLLC/HLL/Roe/Rusanov, MUSCL, and SSP-RK2 - no build step, no dependencies.
Analysis of inviscid flow through a convergent-divergent nozzle (choking, normal/oblique shocks, expansion waves).
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