[en] This document provides the mathematical formulation of the main equations implemented inDARTFlo (https://gitlab.uliege.be/am-dept/dartflo) version 1.3.0, November 2024. For more detailed information about the original implementation, refer to the author's PhD thesis (https://hdl.handle.net/2268/251906). Additionally, more details about the mathematical foundation can be found in the journal article (https://hdl.handle.net/2268/301884).
This theory manual and quick reference guide is organized as follows. Section 1 presents the formulation of the discretized full potential equation and the mesh morphing laws. Section 2 presents the formulation of their partial gradients. Section 3 presents the direct and adjoint solution procedures. Finally, section 4 gives an overview of the available API as well as their configuration parameters.
Research Center/Unit :
A&M - Aérospatiale et Mécanique - ULiège
Disciplines :
Aerospace & aeronautics engineering
Author, co-author :
Crovato, Adrien ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
Language :
English
Title :
DARTFlo - Discrete Adjoint for Rapid Transonic Flows
Publication date :
October 2021
Creation date :
2021-10
Version :
1.3.0
Technical description :
C++/Python finite element code to quickly solve transonic potential flows for preliminary aircraft design and optimization
