123 skills found · Page 1 of 5
mdolab / AdflowADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
brihernandez / SimpleWingsA simple, configurable aerodynamic wing that applies lift at its location. Includes flyable example plane.
addmix / Godot Aerodynamic PhysicsNo description available
GuidodiPasquo / AeroVECTORModel Rocket Simulator oriented to the design and tuning of active control systems, be them in the form of TVC, Active Fin Control or just parachute deployment algorithms on passively stable rockets. It is able to simulate non-linear actuator dynamics and has some limited Software in the Loop capabilities. The program computes all the subsonic aerodynamic parameters of interest and integrates the 3DOF Equations of Motion to simulate the complete flight.
jrgenerative / Fixed Wing SimMatlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.
cfsengineering / CEASIOMpyAerodynamic multidisciplinary design and optimization framework. (Source-Available: Free for academic/evaluation; License required for Commercial/HPC/Cloud use.)
usuaero / MachUpXFast and accurate aerodynamic modeling using general numerical lifting-line theory.
IDEALLab / Airfoil Opt GanExperiment code associated with our paper: "Aerodynamic Design Optimization and Shape Exploration using Generative Adversarial Networks"
yang7857854 / F2AF2A is an aero-hydro-servo-elastic tool developed based on AQWA by Yang Yang, a postdoctoral research associate in Liverpool John Moores University for performing fully coupled analysis of floating offshore wind turbines (FOWT). The aero-servo-elastic simulation capabilities are fully implemented within the user_force64.dll which is a built-in DLL of AQWA for external force calculation. For a coupled analysis of a floating offshore wind turbine subjected to wind, wave and current loadings, the aerodynamic loads acting on the rotor, the elastic responses of the blades and tower, and the servo-control are examined through the DLL, considering the influence from the platform motions. The platform position, velocity and acceleration at each degree of freedom are passed into the DLL to update the kinematics of the upper structures. Before being passed into DLL, these terms are transformed from the inertial coordinate system to the local coordinate system of the platform.
NLRWindSystems / CCBladeA blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superlinear convergence rate), and smooth (continuously differentiable).
usuaero / PylotA fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.
GTSL-UC / T Blade3T-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.
jude-pinkman / Hypercar Sim🏎️ Hypercar Performance Simulator A full-stack physics-based racing simulator built with FastAPI and HTML/CSS/JavaScript. It models real-world drag racing using aerodynamic drag, rolling resistance, torque curves, and gear ratios to simulate hypercar performance. Features multiple race modes, advanced vehicle tuning (engine stages, tires, aero,
NLRWindSystems / AirfoilPreppyA Python module for preprocessing and evaluating aerodynamic airfoil data---primarily for wind turbine applications.
usuaero / MachLineA modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
Saakaarb / Deep Learning For Aerodynamic PredictionThis repository contains code used to create and train a deep neural network that replicates a RANS solver for aerodynamic prediction over airfoils.
brodeau / AerobulkAeroBulk is a modern-FORTRAN-based package/library that gathers state-of-the-art aerodynamic bulk formulae algorithms used to compute turbulent air-sea fluxes of momentum, heat and freshwater.
WyllDuck / OpenFOAM ToolChain For Rocket Aerodynamic AnalysisThis project provides a complete toolchain for evaluating different rocket geometries at subsonic, transonic, and supersonic regimes. The work contained in this repository is part of a student project carried out at the Technical University of Munich (TUM) under the Master of Science (M.Sc) in Aerospace (year 2023).
ZeeshanIqbalKhan / AirfoilANNOfficial repository of paper, entitled "Airfoil’s Aerodynamic Coefficients Prediction using Artificial Neural Network".
YANG-DEMIN / DATCOM ToolsBased on the 1976 USAF STABILITY AND CONTROL DIGITAL DATCOM PROGRAM, the tool is designed to provide a simpler AND more convenient form input with 3d mapping AND aerodynamic characteristics output.
