Youwei-He's Stars
rougier/scientific-visualization-book
An open access book on scientific visualization using python and matplotlib
pytorch/botorch
Bayesian optimization in PyTorch
anyoptimization/pymoo
NSGA2, NSGA3, R-NSGA3, MOEAD, Genetic Algorithms (GA), Differential Evolution (DE), CMAES, PSO
BIMK/PlatEMO
Evolutionary multi-objective optimization platform
yzy1996/English-Writing
Enhance Your English Writing for Science Research 写论文英语素材
peterdsharpe/AeroSandbox
Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
SMTorg/smt
Surrogate Modeling Toolbox
Nek5000/Nek5000
our classic
mdolab/adflow
ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
mdolab/OpenAeroStruct
OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
IDEALLab/airfoil-opt-gan
Experiment code associated with our paper: "Aerodynamic Design Optimization and Shape Exploration using Generative Adversarial Networks"
rvlasveld/oc_svm
One-Class SVM implementations for temporal segmentation of human activities
anyoptimization/pysamoo
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.
h-hg/DDEA
freeSBDO/SBDOT
Surrogate Based Design Optimization Toolbox
yiminzme/awesome-bayesian-optimization
a curated list of bayesian optimization tutorials, papers, softwares
rowan-walsh/CFD-Bayesian-Optimization
Simple Bayesian optimization in MATLAB, with interface to interact with simulations in ANSYS.
flowdiagnosticsitb/KADAL
Kriging for Analysis, Design optimization, And expLoration (KADAL)
aero29/NAX
Non-AXisymmetric aerodynamic design system for turbomachinery
nrsolo/multall-open-gui
An small uni project to create a GUI for the multall-open suite.
RoydeZomer/CEGO
Constrained Efficient Global Optimization algorithm
CircuitGrove/DuctedFanDesignLibrary
An electric ducted fan design library written in Python using the Blender API. Currently, the software is in script form, but an add-on of sorts is being created.
rajatsen91/MFTREE_DET
Multi-Fidelity Deterministic Optimistic Optimization for Black-Box Functions
belakaria/MF-OSEMO
Youwei-He/MESMO
Matlab implementation of the Max-value Entropy Search for Multi-Objective Bayesian Optimization