Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Edoardo Grande"'
Autor:
Francesca Luzi, Elisa Pannucci, Mariangela Clemente, Edoardo Grande, Silvia Urciuoli, Annalisa Romani, Luigi Torre, Debora Puglia, Roberta Bernini, Luca Santi
Publikováno v:
Molecules, Vol 26, Iss 7, p 2104 (2021)
Oxidative stability of food is one of the most important parameters affecting integrity and consequently nutritional properties of dietary constituents. Antioxidants are widely used to avoid deterioration during transformation, packaging, and storage
Externí odkaz:
https://doaj.org/article/022539fcb8d44806a729fc36475714a2
Publikováno v:
INTER-NOISE and NOISE-CON Congress and Conference Proceedings. 264:270-281
Rotor noise comprises harmonic features, related to the blade passing frequency, as well as broadband noise. Even though an acoustic spectrum yields a frequency-distribution of energy within an acoustic pressure signal, it does not reveal phase-relat
Publikováno v:
AIAA Journal: devoted to aerospace research and development, 60(2)
This paper presents an experimental investigation of a propeller operating at low Reynolds numbers and provides insights into the role of aerodynamic flow features on both propeller performances and noise generation. A propeller operating at a tip Re
Publikováno v:
AIAA Journal: devoted to aerospace research and development, 60(9)
28th AIAA/CEAS Aeroacoustics 2022 Conference
28th AIAA/CEAS Aeroacoustics 2022 Conference
This paper explains the presence and relevance of noise caused by a laminar separation bubble (LSB) on a propeller operating at low-Reynolds number. Microphone measurements of a propeller with both clean and forced boundary layer transition blades ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3b0127986bc8911765a466dd10a2ac1d
https://hdl.handle.net/11583/2976883
https://hdl.handle.net/11583/2976883
Autor:
Stefano Meloni, Elisa de Paola, Edoardo Grande, Daniele Ragni, Luana Georgiana Stoica, Alessandro Di Marco, Roberto Camussi
Publikováno v:
28th AIAA/CEAS Aeroacoustics 2022 Conference
AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022)
AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022)
The present study reports a novel wavelet-based method aimed at separating the noise emitted by a single propeller into two contributions, tonal and broadband. An assessment using two different experimental investigations of propellers operating in d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d15a91d3350b4459e2c4564b0097d273
http://resolver.tudelft.nl/uuid:6b139d33-1054-48ae-a519-3f81d40f9e16
http://resolver.tudelft.nl/uuid:6b139d33-1054-48ae-a519-3f81d40f9e16
Publikováno v:
Aerospace Science and Technology, 123
A noise footprint prediction framework for propeller-driven aircraft which couples an aerodynamic model and several aeroacoustic models is presented in this study. The aerodynamic model is based on the blade element momentum theory, while the aeroaco
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a426d67c6cbc5b3e90cbce07446efc06
https://hdl.handle.net/11583/2976887
https://hdl.handle.net/11583/2976887
Publikováno v:
Aerospace Science and Technology. 125:107086
This paper proposes a CFD/CAA-based approach to predict the aerodynamic performances and tonal/broadband noise radiation of low-Reynolds number propellers at engineering level. Broadband self-noise prediction of low-Reynolds number propellers is part
Publikováno v:
Journal of Physics: Conference Series, 1977(1)
The present study reports an experimental investigation regarding one of the most effective and most studied passive control technique in literature to mitigate the noise pollution radiating by a small drone: the Serrated Trailing Edge (STE). 23 quie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a1743db49d4384f3717ea64b40d73769
http://resolver.tudelft.nl/uuid:ed768831-641f-458d-a848-09bf6bf63486
http://resolver.tudelft.nl/uuid:ed768831-641f-458d-a848-09bf6bf63486
Publikováno v:
Aerospace Science and Technology, 113
Experimental and numerical results of a propeller of 0.3 m diameter operated at 5000 RPM and axial velocity ranging from 0 to 20 m/s and advance ratio ranging from 0 to 0.8 are presented as a preliminary step towards the definition of a benchmark con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5c8ef6d17a387ca84f91a76a0622daba
http://resolver.tudelft.nl/uuid:f7194d08-f1bc-4110-926f-5f22171082f4
http://resolver.tudelft.nl/uuid:f7194d08-f1bc-4110-926f-5f22171082f4
Publikováno v:
Aerospace Science and Technology, 120
This paper presents a computational study of flow incidence effects on the aeroacoustics of a propeller operating at low blade-tip Mach numbers. The numerical flow solution is obtained by using the Lattice-Boltzmann/Very Large Eddy Simulation method,