Alternatives and similar repositories for Genetic-airfoil:

Users that are interested in Genetic-airfoil are comparing it to the libraries listed below

• IDEALLab / airfoil-opt-gan
  Experiment code associated with our paper: "Aerodynamic Design Optimization and Shape Exploration using Generative Adversarial Networks"
  ☆64Updated 8 months ago
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆53Updated 6 months ago
• mid2SUPAERO / GEBTAero
  High-aspect-ratio composite wing nonlinear aeroelastic toolbox
  ☆16Updated 5 years ago
• ZeeshanIqbalKhan / AirfoilANN
  Official repository of paper, entitled "Airfoil’s Aerodynamic Coefficients Prediction using Artificial Neural Network".
  ☆31Updated 11 months ago
• 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 ba…
  ☆49Updated 2 years ago
• WISDEM / CCBlade
  A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…
  ☆47Updated last year
• bennames / AeroComBAT-Project
  Aeroelastic Composite Beam Analysis Tool
  ☆17Updated 8 years ago
• gprieto / airfoil_aerodynamic_optimization
  Aerodynamic optimization of an airfoil using an evolutionary algorithm
  ☆30Updated 7 years ago
• The-Fonz / xfoil-optimization-toolbox
  The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…
  ☆43Updated 7 years ago
• nnmrec / Co-Blade
  Software for Analysis and Design of Composite Rotors
  ☆23Updated 7 years ago
• juri117 / cfd-bwb-airfoil-optimizer
  optimizes an Airfoil for a blended wing body using cfd analysis with su2 and optimization by openMdao
  ☆26Updated last year
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆40Updated 2 years ago
• turbo-sim / AxialOpt
  A MATLAB tool for the mean-line design optimization of axial turbines
  ☆30Updated 3 years ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆14Updated 4 years ago
• alfiyandyhr / transonic-airfoil-optim
  I am doing a surrogate optimization of a transonic airfoil. I am using an artificial neural network as my surrogate model to approximate …
  ☆8Updated 3 years ago
• urban-fasel / FlexWingROM
  ☆18Updated 2 years ago
• Mikekiely / wuFoil
  An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
  ☆23Updated last year
• nasa / airfoil-learning
  ☆35Updated 2 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆86Updated this week
• Ry10 / Kulfan_CST
  Used to get the airfoil coordinates from Kulfan parameters or to get the Kulfan parameters from known airfoil coordinates. Uses the CST …
  ☆9Updated 9 years ago
• dracula-ybp / Class-Shape-Transformation-method
  An airfoil parametric method
  ☆21Updated 6 years ago
• ziliHarvey / CNN-for-Airfoil
  CNN for airfoil lift-to-drag-ratio prediction
  ☆40Updated 5 years ago
• raalf / BEMT
  Blade element momentum theory approach to calculate blade forces at varying inflow angles
  ☆10Updated 5 years ago
• usuaero / AirfoilDatabase
  A Python module for modeling airfoils
  ☆34Updated last year
• mid2SUPAERO / aerostructures
  Mapping, Radial Basis Function, RBF, FSI
  ☆11Updated 4 years ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆25Updated 5 months ago
• vsdsantos / nastran-aeroelasticity
  Some usefull routines for aeroelastic analysis with NASTRAN.
  ☆19Updated 2 years ago
• kumar-sumeet / helinoise
  Post-processing framework to predict rotor noise using PSU-WOPWOP from CAMRAD II simulation results
  ☆13Updated 10 months ago
• curiosityFluids / curiosityFluidsAirfoilMesher
  ☆27Updated 5 years ago
• atharvaaalok / Airfoil-Shape-Optimization-RL
  Airfoil shape optimization using Reinforcement Learning
  ☆14Updated last year