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.
Unstructured grid benchmark
Library for aerodynamic, metrology and physics computations. Same calculations as in ADC and other aircraft computers. This also can be used in flight simulations.
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