yangc-yc

yangc-yc's Stars

• OpenModelica/OpenModelica-doc

  OpenModelica documentation

  Language:TeX626

• OpenModelica/OpenModelica

  OpenModelica is an open-source Modelica-based modeling and simulation environment intended for industrial and academic usage.

  Language:Modelica937317

• usnistgov/REFPROP-wrappers

  Wrappers around NIST REFPROP for languages such as Python, MATLAB, etc.

  Language:Mathematica203132

• frkasper/MacroUtils

  MacroUtils is a collection of high-level APIs in order to make your life easier when writing STAR-CCM+ JAVA macros.

  Language:Java4915

• turbo-sim/AxialOpt

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

  Language:MATLAB3110

• ionutalexandru/TurbomachineryBladeDesigner

  Language:MATLAB186

• nicola-sorace/turbine_blade_designer

  A MATLAB project which calculates optimal turbine blade geometry, given airfoil data and environment parameters. It also calculates a very rough estimation of stresses assuming a hollow blade. Three Python scripts are also included, which import this generated blade data into Blender, qBlade and FreeCAD respectively.

  Language:MATLAB41

• GTSL-UC/T-Blade3

  T-Blade3 VERSION 1.2: T-Blade3 is a general parametric 3D blade geometry builder. The tool can create a variety of 3D blade geometries based on few basic parameters and limited interaction with a CAD system. The geometric and aerodynamic parameters are used to create 2D airfoils and these airfoils are stacked on the desired stacking axis. The tool generates a specified number of 2D blade sections in a 3D Cartesian coordinate system. The geometry modeler can also be used for generating 3D blades with special features like bent tip, split tip and other concepts, which can be explored with minimum changes to the blade geometry. The use of control points for the definition of splines makes it easy to modify the blade shapes quickly and smoothly to obtain the desired blade model. The second derivative of the mean-line (related to the curvature) is controlled using B-splines to create the airfoils. This is analytically integrated twice to obtain the mean-line. A smooth thickness distribution is then added to the airfoil with two options either the Wennerstrom distribution or a quartic B-spline thickness distribution. B-splines have also been implemented to achieve customized airfoil leading and trailing edges.

  Language:Fortran4912

• wangzhengyi/TankWar

  用J2SE写的一个坦克大战小游戏，巩固一下java基础

  Language:Java177176

• SUNNERCMS/30daysJavascript

  Javascript 30天的demo来巩固基础

  Language:JavaScript306192

• JackChan1999/Java_Basic_Introduction

  Java基础入门

  727212

• OpenFOAM/OpenFOAM-dev

  OpenFOAM Foundation development repository

  Language:C++1.7k631

• jackfrued/Python-100-Days

  Python - 100天从新手到大师

  Language:Jupyter Notebook163k53.3k

• layumi/2016_person_re-ID

  TOMM2017 A Discriminatively Learned CNN Embedding for Person Re-identification

  Language:C264116

• posenhuang/deeplearningsourceseparation

  Deep Recurrent Neural Networks for Source Separation

  Language:MATLAB368133

• trekhleb/machine-learning-octave

  🤖 MatLab/Octave examples of popular machine learning algorithms with code examples and mathematics being explained

  Language:MATLAB868248

• PRML/PRMLT

  Matlab code of machine learning algorithms in book PRML

  Language:MATLAB6.1k2.2k