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11-parameters-turbine-blade-generator

Parametrization of the geometry of a turbine blade given the 11 parameters as explained in: L.J. Pritchard: An eleven parameter axial turbine airfoil geometry model

adjoint-opt

Shape optimisation of compressor blades using adjoint approach. Implemented in OpenFOAM framework.

ai-edu

AI education materials for Chinese students, teachers and IT professionals.

axialopt

A MATLAB tool for the mean-line design optimization of axial turbines

basicopenfoamprogrammingtutorials

Introduces basic C++ concepts to beginner users of the OpenFOAM open-source CFD libraries.

bimocq

Efficient and Conservative Fluids Using Bidirectional Mapping

blade-geometry

Blade Geometry GUI Written in MATLAB to help Interface with Multall Turbomachinery CFD Solver and Design Tool

bladeblockmesh

Create a wind turbine mesh using blockMesh

ccmd

Centrifugal Compressor Meanline Design

cfd-bayesian-optimization

Simple Bayesian optimization in MATLAB, with interface to interact with simulations in ANSYS.

cfdpython

A sequence of IPython notebooks featuring the "12 Steps to Navier-Stokes" http://lorenabarba.com/

cfview-macro

cimdes

config-2-macros

cooling

Generate cooling hole points placed at airfoils and transfer them from Numeca Autoblade to Ansys CFX

dimensionality_reduction_alo_codes

PCA、LDA、MDS、LLE、TSNE等降维算法的python实现

fucking-algorithm

手把手撕LeetCode题目，扒各种算法套路的裤子。English version supported! Crack LeetCode, not only how, but also why.

hello-world-from-fortran

A case on learning how to control the versions of my codes through github

interpy-zh

📘《Python进阶》（Intermediate Python 中文版）

lfsom

A SOM engine calculator provided with a rich client side

lihang-code

《统计学习方法》的代码实现

loss-measurements-in-a-turbine-cascade

The objective of this report is to evaluate, by measurements, the loss coefficient for a turbine blade row. This experiment has been carried out on a linear non rotating cascade blade row, long enough to disregard the near-wall effects. Tip leaking losses and end wall losses will be disregarded in this experiment. The focus is on the profile losses. The aerodynamic loss coefficient is determined through experimental measures, based on probe transverse measurements. Different parameters, like the inlet angle and the surface roughness, are modified, so that their influence is studied in the process.

mfo-by-matlab

Multi-fan optimization framework by Matlab and ANSYS CFX

multall

Compressor Design Automation

multall-open-18.3

Multall-open is a turbomachinery design system based on the 3D, multistage, Navier-Stokes solver Multall. It can be used to design axial, mixed and radial flow turbines and compressors.

nax

Non-AXisymmetric aerodynamic design system for turbomachinery

numfor

Numeric Modern Fortran

off

OFF, Open source Finite volume Fluid dynamics code

oneflow

LargeScale Multiphysics Scientific Simulation Environment-OneFLOW CFD

optimising-compressor-stage-pso