xflrpy is a python enabled version of xflr5 for scripting and design optimization.

Ahmed bluff body geometry (CAD + STL) and OpenFOAM (v7) validation cases

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).

CFD mesh and model used for « The Process of Making an Aerodynamically Efficient Car Body for the SAE Supermileage Competition » paper.

GPU accelerated vortex filament and vortex particle methods

Simple, but realistic flight simulator controlled by mouse. You can modify aerodynamics of your plane easily by script-like files.

MC-Aero ia an aerodynamic characteristics (drag coefficient and lift coefficient) approximation tool for the full range of angle of attack.

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.

Software for estimating basic aerodynamics characteristics of an aircraft wing.

This rep is mirroring the sail7 code

Unsteady Break-Force 2D

Simulation of transonic flow over a supercritical airfoil using the K-Omega SST Model in OpenFOAM

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.

Simulating Rainfall with openFoam

Shock Estimation Tool

Optimales Flugzeugrumpfdesign durch Topologieoptimierung (Optimizing aircraft fuselage design using topology optimization)

small Wind Turbine Generator System (WTGS) - DIY Project

C++ tool to determine optimal inflation layer growth ratio for CFD boundary layer meshing

3 Dimensional parametric active surface engine developed for Aerodynamic Shape and Topology parametrisation and optimisation.