Massimiliano Nardini

Computational study of the effect of structural compliance on the noise radiated from an elastic trailing-edge

M Nardini, RD Sandberg, SC Schlanderer

Journal article  |  2020  |  Journal of Sound and Vibration

The effect of the structural compliance of an elastic trailing-edge (TE) on its aeroacoustic response is investigated by means of ..

Nonlinear reduced-order modeling of the forced and autonomous aeroelastic response of a membrane wing using Harmonic Balance methods

M Nardini, SJ Illingworth, RD Sandberg

Journal article  |  2019  |  Journal of Fluids and Structures

A nonlinear reduced-order model for a membrane wing at low Reynolds numbers is obtained by coupling a linear aerodynamic model wit..

Reduced-order modeling for membrane wings at low Reynolds numbers

Massimiliano Nardini

Thesis / Dissertation  |  2019

The present work develops reduced-order models for the fluid-structure interaction of two-dimensional membrane wings at low Reynol..

Linear and nonlinear lift frequency response of a pitching membrane wing at low Reynolds numbers

M Nardini, SJ Illingworth, RD Sandberg

Conference Proceedings  |  2018  |  Proceedings of the 21st Australasian Fluid Mechanics Conference, AFMC 2018

A linear state-space reduced-order model for the lift generated by a two-dimensional pitching membrane at low Reynolds numbers is ..

Reduced Order Modeling for Feedback Control of a Flexible Wing at Low Reynolds Numbers

M Nardini, SC Schlanderer, R SANDBERG, S Illingworth

Conference Proceedings  |  2016  |  Journal of Fluids and Structures

A state-space reduced-order model for the lift generated by the unsteady deflection of a two-dimensional flexible wing is presente..