Computational Fluid Dynamics, Waves, Reactions, Plasmas

Python functions for Quasi-1D Gasdynamics

Simple (and not-so-simple) CFD solvers written in Fortran with Python plotting routines

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

A python repository for compressible aerodynamics

Solves the 2D compressible Navier-Stokes equations using finite-difference with a staggered grid arrangement to simulate acoustic waves.

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

Density-based compressible transient solver using the flux difference splitting scheme of Bui, with shock sensor-based upwinding. Primarily designed for compressible LES.

A SageMath library for jump expansions and Jacobian matrices of conservation laws and stability analysis

Code for second order semidiscrete central upwind schemes.

A compressible flow calculator written in Python.

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

Compressible Falkner-Skan-Cooke equation solver

A compact Finite Volume Method solver for 2D Euler equations (internal channel flow). Demonstrates numerical methods, scientific programming and shock capturing.

Modeling performance of GE's F404-GE-402 engine in pyCycle

Compressible potential flow solver

Minimal estimator of ideal (isentropic) rocket nozzle performance: exit state (Me, Pe, Te), CF, Isp, F/At, with Pc–area-ratio sweeps. Pure Python, small tests, CSV output for quick trade studies. Requires Python 3.10+.

SymPy-based lab for quasi-1D nozzle gasdynamics: symbolic isentropic relations, numerical profiles, and engineering plots.

Transient startup of a liquid-fueled rocket nozzle using a 2D axisymmetric compressible-flow. 1.1 MN of thrust

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

SymPy-based lab for 1D vertical rocket mechanics: symbolic equations of motion, Tsiolkovsky Δv, and simple numeric experiments.

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.

🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.