home.md

@@ -3,18 +3,14 @@ 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.
 
 This wiki contains the following documentation:
-- a step by step [build](build) guide
-- a step by step [how-to-use](use) guide
-- some C++ ([dart](dart_cclasses), [tbox](tbox_cclasses)) and [Python](pyclasses) classes documentation
-- a short description of some [additional modules](module)
-- a [benchmark](bench) page
-- a list of [known bugs](bugs)
-
-The documentation for developers can be built with doxygen.
+- [build](build) instructions
+- [use](use) instructions
+- some [additional resources](addition)
+Additionaly, the documentation for developers can be built using doxygen, and the mathematical and numerical formulations of DART can be found in this [Ph.D. thesis](http://hdl.handle.net/2268/251906).
 
 ![](pics/main.png)
 
-## Features and limitations (dart v1.0.0, September 2021)
+## Features and limitations (dart v1.1.0, September 2021)
 * Geometry
   - 2D
     - [x] airfoils
@@ -72,4 +68,4 @@ The documentation for developers can be built with doxygen.
 ## Envisioned developments
 * Addition of [CPACS](https://cpacs.de/) or [OpenVSP](http://openvsp.org/) to gmsh geometry interface
 * Extension to unsteady flow with linear harmonic perturbations methods
-* Extension of viscous-inviscid interaction to 3D transonic flows
\ No newline at end of file
+* Extension of viscous-inviscid interaction to 3D transonic flows