usuaero / MachLine

A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.

Date Created 2022-01-10 (2 years ago)

Commits 1,002 (last one about a month ago)

Stargazers 33 (0 this week)

Watchers 3 (0 this week)

Forks 4

License mit

Ranking

RepositoryStats indexes 584,353 repositories, of these usuaero/MachLine is ranked #546,732 (6th percentile) for total stargazers, and #422,423 for total watchers. Github reports the primary language for this repository as Fortran, for repositories using this language it is ranked #348/366.

usuaero/MachLine is also tagged with popular topics, for these it's ranked: cfd (#102/104)

Other Information

usuaero/MachLine has Github issues enabled, there is 1 open issue and 8 closed issues.

All Topics

cfd subsonic panel-code supersonic aerodynamics panel-method inviscid-flow panel-methods supersonic-flow incompressible-flow unstructured-meshes low-order-aerodynamics

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Recent Commit History

847 commits on the default branch (main) since jan '22

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Languages

The primary language is Fortran but there's also others...

updated: 2024-11-21 @ 11:03am, id: 446548209 / R_kgDOGp3I8Q