JAX-Based GPU-Accelerated CFD calculations on 2D Rotating Detonation Combustors

Development of quasi-one dimensional scramjet combustor code using real gas equations and NASA CEA code

This project implements a sophisticated optimization algorithm for small-scale ramjet engine design, with particular focus on achieving stable supersonic combustion and optimal shock wave patterns.…

Code to extract, process and analyse data from traversing gas probe, thermocouple and stationary DSLR camera on the Flameless Combustor at the Clean Combustion Laboratory, Faculty of Aerospace Engi…

One dimensional method that simulates dual-mode Scramjet isolator-combustor in Fortran

A python wrapper for Tavily search API

PaSR-SDE is a code to simulate premixed turbulent combustion in a partially stirred reactor using stochastic mixing models.

Efficient approach for evaluating the sensitivity of ignition delay time. Implement with Cantera/Python

Python wrapper to do sensitivity analysis with CHEMKIN-Pro

Numeric solver to predict missile flight performance

This project models the steady-state behavior of three different types of aircraft engines: turbojet, turbofan and ramjet. It allows the study of their performance at different operating conditions.

A collection of scripts /etc for my 3rd Year Individual Project, building a supersonic ramjet (NOT a SCRAMJET)

MATLAB function for the optimization of a ramjet propulsion system and some associated aircraft propulsion functions

Model flow through Ramjet engine

This MATLAB script performs a parametric study on the ramjet/scramjet propulsion performance. Several key parameters are varied throughout the script. The script runs the function file Ramjet.m for…

Analyses the variation of propulsive and thermodynamic efficiency for a ramjet engine with various input parameters

An OpenFOAM function object to compute finite-time Lyapunov exponent (FTLE) fields during any OpenFOAM (FOAM-extend) CFD simulation

Collection of Matlab functions for Reduced-Order Modelling (ROM) of combustion data sets.

Using differential diffusion transport in OpenFOAM-10

Combustion Modeling - Iran First International Combustion School (ICS2019)

A MATLAB-GUI based open-source tool for solving gaseous combustion problems

Parallel Programming Project for Simution of Supersonic Combustion

Project design for a simple sc/ramjet

Designing a ramjet rocket engine whose intake comprises double-angle wedges to maximize total pressure recovery for different flight conditions

Designing a ramjet engine using first principles of compressible flow. Components simulated include: inlet, diffuser, flameholder, combustor, converging and diverging nozzle.