A MATLAB-based framework for solving combustion and high-speed flow problems

Reliable compressible-flow calculator with batch CSV runs, automated reports, and validation-aware shock/isentropic analysis.

Aynı Ailden 2 Şok Dalgasının Kesişmesi Sonucu Oluşacak Akışın Genel Özelliklerini Hesaplamaktadır.

To model supersonic flow around a bullet, calculate Cd and drag forces using MATLAB, and validate these with Fluent CFD simulations, comparing analytical and numerical approaches for accuracy.

Repository for Bachelor of Science thesis "Computer simulations of shock wave propagation within kinetic Monte Carlo method"

MATLAB ENAE488P hypersonic flow coursework and project scripts, including a hypersonic caret waverider analysis/design study.

纯前端气动/流体力学计算器,含标准大气、等熵流、正/斜激波与一维黎曼精确解,带交互图表。 | Browser-based aerospace & compressible-flow calculator: standard atmosphere, Sutherland viscosity, isentropic flow, normal/oblique shocks, and exact 1D Riemann solver — pure front-end with interactive charts.

Mach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.

It calculates the general properties of the flow that will occur as a result of the intersection of two shock waves from the same family.

C++ code for Rado Faletič’s tomographic routines used in his PhD thesis.