A MATLAB-based framework for solving combustion and high-speed flow problems
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Updated
Jun 26, 2026 - MATLAB
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.
Lagrangian particle tracking for compressible CFD data. Quantifies tracer-inertia bias in supersonic PIV by tracking particles through PLOT3D flow fields under nine drag closures.
COmpressible Multiphase multiPhysics Adaptive Solver
Aynı Ailden 2 Şok Dalgasının Kesişmesi Sonucu Oluşacak Akışın Genel Özelliklerini Hesaplamaktadır.
RANS/SST k–ω CFD study of surface roughness effects on oblique shock formation over a double-wedge model in supersonic flow
Python check of divergent nozzle wall profiles: 1-D validity (wall angle vs Prandtl-Meyer angle) and Mach-wave shock estimate. MachViz team project, OVGU
Repository for Bachelor of Science thesis "Computer simulations of shock wave propagation within kinetic Monte Carlo method"
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.
Mach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.
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.
Idealized reduced-order model of blast-fishing shocks on coral skeleton beneath a gas-laden canopy, with exact layered-acoustics solvers, Keller-Miksis bubble dynamics, 2D FDTD, and verified closed forms.
MATLAB ENAE488P hypersonic flow coursework and project scripts, including a hypersonic caret waverider analysis/design study.
Mollified-sharp decomposition and POD-GPR modeling for transonic RAE2822 flows
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.
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