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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 supervised by Assoc. Prof. Torsten Schenkel, the software is meant to allow users to easily compute axisymmetric rocket nozzles utilizing the iterative Axisymmetric Method of Characteristics (MOC) procedure. The methodology is thoroughly described in the paper: LINK COMING SOON.

clawpack

Package for solving hyperbolic systems of partial differential equations

finite-volume-solver

Final Project for course 250D at UCLA. Source code and report provided. THe project was a 2 dimensional finite volume solver for supersonic flow in a jet inlet. The application was finding oblique shocks. Used MacCormacks Method with artificial dissipation.

hypersonics_fromshockwaves2scramjets

ldc

The LLVM-based D Compiler.

method_of_characteristics

This is a simple MOC code written in MATLAB calculating the characteristics and Mach number distribution for a simple turn.

moc

Method of Characteristics code in Python

moc-1

C++ implementation of a method of characteristics for nozzle analysis with supersonic flow.

moca

MoCA - Method of Characteristics for Axisymmetric flows

nozzledesign

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

openmoc

A method of characteristics code for nuclear reactor physics calculations.

propprelib

A library to assist with MATLAB functions for Propulsion Prelim

pytorch-handbook

pytorch handbook是一本开源的书籍，目标是帮助那些希望和使用PyTorch进行深度学习开发和研究的朋友快速入门，其中包含的Pytorch教程全部通过测试保证可以成功运行

ramjet-analysis-aircraft-propulsion

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 each study.

rocket_nozzle_design

Method of characteristics (MoC) code for the design of a rocket nozzle (diverging section), with comparison to quasi-1D results.

soton-nozzle

Method of Characteristics computation to find geometry of a supersonic nozzle at University of Southampton

su2

SU2: An Open-Source Suite for Multiphysics Simulation and Design

t-mats

An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System, Numerical Methods, Newton-Raphson, Jacobian Calculation, Propulsion, Aircraft Engine, Jet, Turbofan, Turbojet, Compressor, Turbine, Nozzle, Inlet, open source

tensorflow

Computation using data flow graphs for scalable machine learning

tensorflow-tutorial

Example TensorFlow codes and Caicloud TensorFlow as a Service dev environment.

three-dimensional-nozzle-design-code