Linear and Nonlinear Reduced Order Models for Sloshing for Aeroelastic Stability and Response Predictions

Linear and Nonlinear Reduced Order Models for Sloshing for Aeroelastic Stability and Response Predictions

This paper makes use of sloshing reduced-order models to investigate the effects of sloshing dynamics on aeroelastic stability and response of flying wing structure. More specifically, a linear frequency-domain operator derived by an equivalent mechanical model is used to model lateral (linear) slos...

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Bibliographic Details
Main Authors: Marco Pizzoli, Francesco Saltari, Franco Mastroddi
Format: Article
Language:English
Published: MDPI AG 2022-08-01
Series:Applied Sciences
Subjects:
flexible aircraft
aeroelasticity
linear and nonlinear sloshing
equivalent mechanical models
neural networks
Online Access:https://www.mdpi.com/2076-3417/12/17/8762

Internet

https://www.mdpi.com/2076-3417/12/17/8762

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