A parametric aircraft geometry tool
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Updated
Sep 30, 2025 - C
A parametric aircraft geometry tool
DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization
Computational Fluid Dynamics, Waves, Reactions, Plasmas
A code based on the Finite Volume Method discretisation of Navier-Stokes equations for simulation of compressible shear layer
AeroTop: an efficient aerodynamic topology optimization framework
This project outputs G-code that is used to control a 4-axis hot wire cutter, employed to cut a wing / airfoil from a physical block of foam. Effectively, it is a slicer for a particular arrangement of raw-coordinate data files.
A pure C implementation of the QPROP algorithm for analyzing the aerodynamic performance of propellers, with Python/MATLAB/Julia interfaces
Unstructured grid benchmark
Run AoA sweeps automatically, compute forces and coefficients (Cl, Cd), and export results for post‑processing.
Library for aerodynamic, metrology and physics computations. Same calculations as in ADC and other aircraft computers. This also can be used in flight simulations.
Simulator of flight with LODed landscape using old OpenGL
🤖 Optimize C code efficiently with AI to achieve up to 3.4× faster performance compared to human-written code and standard compiler optimizations.
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