AIAA AVIATION 2022 Forum 2022
DOI: 10.2514/6.2022-3595
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Free Wake Panel Method Simulations of a Highly Flexible Wing at Flutter

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Cited by 4 publications
(3 citation statements)
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“…At the moment, our implementation was compared to an open-source C++ panel code (Baayen, 2012), and we observed speedup of over an order of magnitude. The method also supports large displacement aeroelasticity (Ribeiro et al, 2022a), although this is not included in this work.…”
Section: Methodsmentioning
confidence: 99%
“…At the moment, our implementation was compared to an open-source C++ panel code (Baayen, 2012), and we observed speedup of over an order of magnitude. The method also supports large displacement aeroelasticity (Ribeiro et al, 2022a), although this is not included in this work.…”
Section: Methodsmentioning
confidence: 99%
“…We employ a source and doublet panel method with free wake modelling [8]. The code employed in this work was recently validated for moving airfoils and wind turbine rotors [9], including several dynamic effects [10] and flexible wing aeroelasticity [11]. The thickness effects are fully captured, as the triangular or quadrilateral panels lie on the blade surfaces.…”
Section: Methodsmentioning
confidence: 99%
“…At the moment, our implementation was compared to an open source C++ panel code (Baayen, 2012) and we observed over an order of magnitude in speed up. The method also supports large displacement aeroelasticity (Ribeiro et al, 2022a), although this is not included in this work.…”
Section: Methodsmentioning
confidence: 99%