Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Renato Fuzaro Miotto"'
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
William Wolf, Renato Fuzaro Miotto
Publikováno v:
Procceedings of the 18th Brazilian Congress of Thermal Sciences and Engineering.
Publikováno v:
Journal of sound and vibration, 407, 253-270. Academic Press
Based on Amiet's theory formalism, we propose a numerical framework to compute the aeroacoustic transfer function of realistic airfoil geometries. The aeroacoustic transfer function relates the amplitude and phase of an incoming periodic gust to the
Autor:
André V. G. Cavalieri, José Rodrigues de Lima Neto Sirotto, William Wolf, Julio A. Cordioli, Petrônio A. S. Nogueira, Renato Fuzaro Miotto
Publikováno v:
The Journal of the Acoustical Society of America. 146(1)
Acoustic measurements of turbulent jets in the vicinity of a flat plate, mimicking a neighbouring wing, were compared to results from two wavepacket-based source models previously studied in the literature: the Tailored Green's Function method, which
Publikováno v:
2018 AIAA/CEAS Aeroacoustics Conference
In this paper, three different techniques are combined to provide a complete physics-based semi-anytical model for leading-edge noise prediction. The model is based on the classical theory of Amiet. Here, the two-dimensional turbulence spectrum is co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c093d91d783377f360f7d9c22b250961
http://www.scopus.com/inward/record.url?scp=85051285965&partnerID=8YFLogxK
http://www.scopus.com/inward/record.url?scp=85051285965&partnerID=8YFLogxK
Autor:
André V. G. Cavalieri, José Rodrigues de Lima Neto Sirotto, Petrônio A. S. Nogueira, Renato Fuzaro Miotto, William Wolf, Julio A. Cordioli
Publikováno v:
2018 AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
AIAA journal, 56(5), 1711-1716. American Institute of Aeronautics and Astronautics Inc. (AIAA)
This paper presents a study of the leading-edge noise radiated by an airfoil undergoing a turbulent inflow. The noise prediction of generic airfoil profiles subjected to spanwise-varying inflow conditions is performed with the support of Amiet’s th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b97cb98d259b6be7fd44dd76dcd8a041
https://research.utwente.nl/en/publications/ce0b6f4f-3566-42d1-a684-4632ce8bc1cf
https://research.utwente.nl/en/publications/ce0b6f4f-3566-42d1-a684-4632ce8bc1cf
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference, 2017
We propose a numerical framework to compute the airfoil-gust lift response and its subsequent leading-edge noise generation due to an incident compressible turbulent flow. This approach is valid for blades with large aspect ratios, general airfoil ge
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c131a287db3dfa108f5f20df18835b00
https://research.utwente.nl/en/publications/954aa581-c4af-462b-bf2f-7b6d5ebe44df
https://research.utwente.nl/en/publications/954aa581-c4af-462b-bf2f-7b6d5ebe44df
Autor:
William Wolf, Renato Fuzaro Miotto
Publikováno v:
Procceedings of the 24th ABCM International Congress of Mechanicl Engineering.