- VLM
- NL-VLM
- UVLM
- NL-UVLM
- NLHB-UVLM
- High angle of attack correction
- Dihedral / Anhedral Wings (local coordinate projection in force calculation)
- Swept Wings (coordinate rotation)
- Compressibility Effects (Prandtl Glauert corrector)
- ISPC
- CUDA
- Clangd
- Clang-Format
- Clang-Tidy
- Testing framework (via
xmake test
) - Compilation CI
- Documented code (doxygen style)
Requirements:
- Windows (MSVC compiler) or Linux (GCC or Clang)
- xmake build system
- For Windows, the installer is recommended
- For Linux, run
curl -fsSL https://xmake.io/shget.text | bash
Then build and run the default config:
xmake -y -v && xmake run
The solver should run and output the aerodynamic coefficients along with some time metrics:
reading plot3d mesh
number of panels: 4096
ns: 64
nc: 64
LHS: 12.106 ms
RHS: 4 us
Solve: 341.976 ms
Compute forces: 104 us
>>> Alpha: 5.0 | CL = 0.464887 CD = 0.005636 CMx = 1.157476 CMy = -0.017555 CMz = 0.101128
SOLVER RUN: 358.235 ms