@@ -3,11 +3,11 @@ DARTFlo (Discrete Adjoint for Rapid Transonic Flows, abbreviated as DART) is an
DART is currently capable of rapidly solving steady transonic flows on arbitrary configurations, ranging from 2D airfoils to 3D full aircraft (without engine), as well as calculating the flow gradients using a discrete adjoint method. Furthemore, the code is interfaced with [CUPyDO](https://github.com/ulgltas/CUPyDO) and [openMDAO](https://openmdao.org/) so that aeroelastic computations and optimization can be easily carried out.
The wiki contains the documentation related to users:
-[C++](dart_cclasses) and [Python](dart_pyclasses) classes documentation
- a step by step [how-to-use](dart_usage) guide
- a short description of some [additional modules](dart_mod)
- a list of [known bugs](dart_bugs)
- a [benchmark](dart_bench) page
-[C++](dart_cclasses) and [Python](pyclasses) classes documentation
- a step by step [how-to-use](use) guide
- a short description of some [additional modules](module)
- a list of [known bugs](bugs)
- a [benchmark](bench) page
The documentation for developers can be built with doxygen.
