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In this Thesis, numerical panel methods are used to investigate the critical flutter conditions of an flexible AGARD wing immersed in unsteady transonic flow, and the results are compared to experimental data, given by AGARD.

In this Thesis, numerical panel methods are used to investigate the critical flutter conditions of an flexible AGARD wing immersed in unsteady transonic flow, and the results are compared to experimental data, given by AGARD.

MODELLAZIONE NUMERICA AEROELASTICA DI ALI FINITE VIBRANTI IN UN FLUSSO TRANSONICO NON STAZIONARIO PER LA PREDIZIONE DELLE CONDIZIONI DI FLUTTER

LARASPATA, VITO
2022/2023

Abstract

In this Thesis, numerical panel methods are used to investigate the critical flutter conditions of an flexible AGARD wing immersed in unsteady transonic flow, and the results are compared to experimental data, given by AGARD.
2022
NUMERICAL AEROELASTIC MODELING OF FINITE WINGS VIBRATING IN UNSTEADY TRANSONIC FLOW FOR THE PREDICTION OF FLUTTER CONDITIONS
In this Thesis, numerical panel methods are used to investigate the critical flutter conditions of an flexible AGARD wing immersed in unsteady transonic flow, and the results are compared to experimental data, given by AGARD.
SORIA, LEONARDO
DIMITRIADIS, GRIGORIOS
Lauree magistrali a ciclo unico
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14253/64942