AIAA Scitech 2021 Forum 2021
DOI: 10.2514/6.2021-1037
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Uncertainties Quantification in Flutter Prediction of a Wind Tunnel Model Exhibiting Large Displacements

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Cited by 7 publications
(2 citation statements)
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“…Several groups have simulated the Pazy wing, typically using nonlinear static and linearized dynamic simulations (Ritter et al, 2021), as adding both static and dynamic structural and aerodynamic nonlinearities concurrently is considered demanding (Righi, 2021). The linearization needs to be done on the deformed configuration, i.e., after statically deforming the wing for certain flow conditions, to deal with the wing static nonlinearities (Goizueta et al, 2022).…”
Section: Phase Between Wing Tip Displacement and Gust Vertical Velocitymentioning
confidence: 99%
“…Several groups have simulated the Pazy wing, typically using nonlinear static and linearized dynamic simulations (Ritter et al, 2021), as adding both static and dynamic structural and aerodynamic nonlinearities concurrently is considered demanding (Righi, 2021). The linearization needs to be done on the deformed configuration, i.e., after statically deforming the wing for certain flow conditions, to deal with the wing static nonlinearities (Goizueta et al, 2022).…”
Section: Phase Between Wing Tip Displacement and Gust Vertical Velocitymentioning
confidence: 99%
“…Several groups have simulated the Pazy wing, typically with linearized methods [6], as adding structural and aerodynamic non-linearities is considered demanding [7]. The linearization needs to be done on the deformed configuration, i.e., after statically deforming the wing for certain flow conditions, to deal with the aforementioned non-linearities [8].…”
Section: Introductionmentioning
confidence: 99%