xflrpy is a python enabled version of xflr5 for scripting and design optimization.
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Updated
Oct 4, 2025 - C++
xflrpy is a python enabled version of xflr5 for scripting and design optimization.
This 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).
Ahmed bluff body geometry (CAD + STL) and OpenFOAM (v7) validation cases
GPU accelerated vortex filament and vortex particle methods
CFD mesh and model used for « The Process of Making an Aerodynamically Efficient Car Body for the SAE Supermileage Competition » paper.
Simple, but realistic flight simulator controlled by mouse. You can modify aerodynamics of your plane easily by script-like files.
Simulation of transonic flow over a supercritical airfoil using the K-Omega SST Model in OpenFOAM
Software for estimating basic aerodynamics characteristics of an aircraft wing.
Code and Design files for hovering ornithopter MAV 🐦
A powerful and rapid data interpolator.
MC-Aero ia an aerodynamic characteristics (drag coefficient and lift coefficient) approximation tool for the full range of angle of attack.
Mechanical and Aerospace Engineering Final Year Project
small Wind Turbine Generator System (WTGS) - DIY Project
Pitch of an aircraft is controlled by the elevator which is situated at the rare of the airplane running parallel to the wing that houses the ailerons. Pitch control is a longitudinal problem, and this repository presents the design of an Arduino-based system as a solution.
OpenFoam case file for 2D simulation of external flow across a shape
High Performance CPU/GPU Potential Flow Solver
Program translates MSC Nastran Cquad elements with 1D Crod on leading edge to CAERO1 elements with generation of d2wgj, wkk and f2gj matricles.
An aerodynamic analysis tool that determines the transient and steady-state behavior of a propeller in autorotation, given its geometry and initial crossflow conditions.
Optimales Flugzeugrumpfdesign durch Topologieoptimierung (Optimizing aircraft fuselage design using topology optimization)
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