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2d-minimum-length-nozzle

Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.

aerospike-nozzle-design-gui

Graphical software for designing aerospike rocket nozzles

aerospikedesign

Design of a regeneratively cooled aerospike nozzle for UTAT for APS490Y

aerospikes-fan

A fan with aerospike nozzle that powered by Bambu Lab X1C toolhead turbo

ansys_cfx

VSCode extension for ANSYS CFX Command Language (CCL) and CFD Post State (.cst) language support

axisymmetric-method-of-characteristics-nozzle-designer-with-gui

This programme was developed in conjunction with a paper on the matter named "A Detailed Presentation and Implementation Procedure of Axisymmetric Method of Characteristics for Rocket Nozzle Design". Developed by Kyril Palaveev and Dr. Torsten Schenkel, the software is meant to allow users to easily compute axisymmetric rocket nozzles utilizing the

bell-nozzle

This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.

characteristicmethod

Characteristic Method for 2d Nozzle

chemicalmechanisms

collectionofmechanisms

A data hub for combustion reaction mechanisms

fipy

FiPy is a Finite Volume PDE solver written in Python

fluidx3d

The fastest and most memory efficient lattice Boltzmann CFD software, running on all GPUs via OpenCL.

ignition-delay

Исследование задержки самовоспламенеиня

ldc

The LLVM-based D Compiler.

methodofcharacteristicsnozzle

A custom GUI app for rocket engine design using the Method of Characteristics in C++

methodofmomentssootmodel

Method of Moments soot model for ANSYS FLUENT 17.2

moc-matlab

Method of Characteristics for Nozzle Design

nasa-latex-docs

An easy and convenient package to create technical LaTeX documents.

navier-stokes-2d-numerical-solve-incompressible-flow-with-custom-scenarios-matlab-

I have created this repository to share my code for 2D numerical solving of Navier stokes equations (incompressible flow); although it will take a little time for me to completely update the repository

nozzle_design

A design process for a bell nozzle, based on the method of characteristics (MOC), and written in Matlab .

nozzle_moc_supersonic

A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle

nozzledesign

Script to design minimum length supersonic nozzle for a given design exit Mach number using Method of Characteristics

nozzledesign-1

Implement method of wave declination to design a Supersonic Nozzle

nozzlesim

Uses the method of characteristics to simulate supersonic flow in an axisymmetric nozzle, and use Busemann's method to construct a nozzle producing isentropic flow according to certain parameters

odt

openfoam-sonicfoam-2d-merlin-nozzle-4

This Repository contains everything needed to complete a basic CFD analysis of a Rocket Nozzle cross section. The analysis will be performed using the basic specifications from a SpaceX Merlin 1D engine

propprelib

A library to assist with MATLAB functions for Propulsion Prelim

radlib

Radiation property library for combustion gases and soot

rgp-gen

Real Gas Property File Generator for ANSYS CFX V14.5

rocketcea

RocketCEA Wraps The NASA Fortran CEA Code