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- [use](use) instructions
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- some [additional resources](addition)
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Additionally, the documentation for developers can be built using doxygen. The mathematical and numerical formulations of DART can be found in [this Ph.D. thesis](http://hdl.handle.net/2268/251906), and in [this technical note](http://hdl.handle.net/2268/264284).
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Additionally, the documentation for developers can be built using doxygen. The mathematical and numerical formulations of DART can be found in [this technical note](http://hdl.handle.net/2268/264284). Main scientific publications are also listed at the bottom of the page.
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| ... | ... | @@ -46,9 +46,9 @@ Additionally, the documentation for developers can be built using doxygen. The m |
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- [x] Eigen's GMRES
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- [x] MUMPS
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- Wake/Kutta condition
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- [x] direct matrix manipulation (see [Nishida, 1996](https://dspace.mit.edu/handle/1721.1/11188), [Galbraith, 2017](https://arc.aiaa.org/doi/abs/10.2514/6.2017-0290) and [Crovato, 2020](http://hdl.handle.net/2268/251906))
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- [x] direct matrix manipulation (see [Nishida, 1996](https://dspace.mit.edu/handle/1721.1/11188), [Galbraith, 2017](https://arc.aiaa.org/doi/abs/10.2514/6.2017-0290) and [Crovato, 2021](https://hdl.handle.net/2268/264284))
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- Artificial viscosity
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- [x] best upstream alignment (see [Crovato, 2020](http://hdl.handle.net/2268/251906))
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- [x] best upstream alignment (see [Crovato, 2021](https://hdl.handle.net/2268/264284))
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- [x] adaptive
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* Post-processing
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- Data extracted at nodes
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## Envisioned developments
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* Addition of [CPACS](https://cpacs.de/) or [OpenVSP](http://openvsp.org/) to gmsh geometry interface
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* Extension to unsteady flow with linear harmonic perturbations methods
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* Extension of viscous-inviscid interaction to 3D transonic flows |
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* Extension of viscous-inviscid interaction to 3D transonic flows
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## References
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* Crovato Adrien, [DARTFlo - Discrete Adjoint for Rapid Transonic Flows](https://hdl.handle.net/2268/264284), Technical note, University of Liège, 2021.
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* Crovato Adrien, [Steady Transonic Aerodynamic and Aeroelastic Modeling for Preliminary Aircraft Design](https://hdl.handle.net/2268/251906), PhD thesis, University of Liège, 2020.
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* Crovato A., et al. [A discrete adjoint full potential formulation for fast aerostructural optimization in preliminary aircraft design](https://orbi.uliege.be/handle/2268/301884), Aerospace Science and Technology, 2023.
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* Crovato A., et al., [A Full Potential Static Aeroelastic Solver for Preliminary Aircraft Design](https://hdl.handle.net/2268/237955), Proceedings of the 18th International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2019.
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* Crovato A., et al., [Fast Full Potential Based Aerostructural Optimization Calculations for Preliminary Aircraft Design](https://hdl.handle.net/2268/292456), Proceedings of the 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2022. |
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