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Sodja, J. (author), De Breuker, R. (author), Nozak, Dejan (author), Drazumeric, Radovan (author), Marzocca, Pier (author)Low-fidelity fluid–structure interaction model of flexible propeller blades is assessed by means of comparison with high-fidelity aeroelastic results. The low-fidelity model is based on a coupled extended blade-element momentum model and non-linear beam theory which were both implemented in Matlab. High-fidelity fluid–structure interaction...journal article 2018
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Abbas, L.K. (author), Rui, X. (author), Marzocca, P. (author), Abdalla, M. (author), De Breuker, R. (author)In this paper, the effect of the system parameters on the flutter of a curved skin panel forced by a supersonic/hypersonic unsteady flow is numerically investigated. The aeroelastic model investigated includes the third-order piston theory aerodynamics for modeling the flow-induced forces and the Von Kármán nonlinear strain-displacement relation...journal article 2011
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Donnell, K.O. (author), Schober, S. (author), Stolk, M. (author), Marzocca, P. (author), De Breuker, R. (author), Abdalla, M. (author), Nicolini, E. (author), Gürdal, Z. (author)This paper discusses modeling, simulations and experimental aspects of active aeroelastic control on aircraft wings by using Synthetic Jet Actuators (SJAs). SJAs, a particular class of zero-net mass-flux actuators, have shown very promising results in numerous aeronautical applications, such as boundary layer control and delay of flow separation...conference paper 2007