Zobrazeno 1 - 10
of 155
pro vyhledávání: '"Massimo Gennaretti"'
Publikováno v:
Aerospace, Vol 11, Iss 9, p 745 (2024)
A time-stepping, lifting-line solution algorithm for the prediction of the unsteady aerodynamics of morphing wings is presented. The velocity induced by the wake vorticity is determined through a free-wake vortex-lattice model, whereas the Küssner a
Externí odkaz:
https://doaj.org/article/d176c950b0fc4266bd8ac483515a5575
Publikováno v:
Applied Sciences, Vol 12, Iss 23, p 12204 (2022)
A frequency-domain lifting-line solution algorithm for the prediction of the unsteady aerodynamics of wings is presented. The Biot–Savart law is applied to determine the normalwash generated by the wake vorticity distribution, whereas steady and un
Externí odkaz:
https://doaj.org/article/5c0349001b3344b09643ced53e8ff3cc
Publikováno v:
Applied Sciences, Vol 12, Iss 19, p 9507 (2022)
This paper presents a numerical investigation of noise radiated by two side-by-side propellers, suitable for Distributed-Electric-Propulsion concepts. The focus is on the assessment of the variation of the effects of blade tip Mach number on the radi
Externí odkaz:
https://doaj.org/article/bc42a342edc34519a38f522c37d6cc4f
Autor:
Giovanni Bernardini, Francesco Centracchio, Massimo Gennaretti, Umberto Iemma, Claudio Pasquali, Caterina Poggi, Monica Rossetti, Jacopo Serafini
Publikováno v:
Applied Sciences, Vol 10, Iss 8, p 2643 (2020)
This paper presents an investigation of the aerodynamic and aeroacoustic interaction of propellers for distributed electric propulsion applications. The rationale underlying the research is related to the key role that aeroacoustics plays in the esta
Externí odkaz:
https://doaj.org/article/604765d0a16e4f49aad25897c0ee76f5
Publikováno v:
International Journal of Aerospace Engineering, Vol 2017 (2017)
The aim of this paper is the evaluation of several pilot models found in the literature, suited for helicopter pilot-assisted and pilot-induced oscillations analyses. Three main topics are discussed: (i) sensitivity of rotorcraft-pilot couplings simu
Externí odkaz:
https://doaj.org/article/a7a1d76eb318495d874afac8b03baf3d
Publikováno v:
International Journal of Aerospace Engineering, Vol 2015 (2015)
The aim of this paper is the assessment of the capability of controllers based on the combined actuation of flaps and variable-stiffness devices to alleviate helicopter main rotor vibratory hub loads. Trailing-edge flaps are positioned at the rotor b
Externí odkaz:
https://doaj.org/article/e82a6a30a2cc4b7aaf8f8625516698eb
Autor:
Massimo Gennaretti, Riccardo Giansante
Publikováno v:
AIAA Journal. 60:5779-5790
This paper presents the extension of the Kutta–Joukowski theorem to unsteady linear aerodynamics. Starting from the formulation developed by Theodorsen for the solution of the velocity potential for circulatory flows around thin, rectilinear airfoi
This paper deals with the development and application of an algorithm aimed at the identification of open-loop transfer functions from closed-loop data. Particularly suited for helicopter applications, it allows the identification of the machine tr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3668::b6b9882780dfb886c3600a42c276f690
https://hdl.handle.net/11590/417267
https://hdl.handle.net/11590/417267
Autor:
Caterina Poggi, Monica Rossetti, Jacopo Serafini, Giovanni Bernardini, Massimo Gennaretti, Umberto Iemma
Publikováno v:
Aerospace Science and Technology. 130:107910
Publikováno v:
AIAA AVIATION 2021 FORUM.