Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Adson Agrico de Paula"'
Autor:
William Denner Pires Fonseca, Rafael Rosario Da Silva, Reinaldo Marcondes Orselli, Adson Agrico de Paula, Ricardo Galdino da Silva
Publikováno v:
Revista Facultad de Ingeniería Universidad de Antioquia, Iss 98 (2021)
In this work, a numerical study of flow around an airfoil with wavy leading Edge is presented at a Reynolds number of 3X106. The flow is resolved by considering the RANS (Reynolds Average Navier-Stokes) equations. The baseline geometry is based on th
Externí odkaz:
https://doaj.org/article/ba6523f12c6e4576ba2b1bcdf103e185
Autor:
William Denner Pires Fonseca, Rafael Rosario Da Silva, Reinaldo Marcondes Orselli, Adson Agrico de Paula, Ricardo Galdino da Silva
Publikováno v:
Revista Facultad de Ingeniería Universidad de Antioquia, Issue: 98, Pages: 69-77, Published: MAR 2021
In this work, a numerical study of flow around an airfoil with wavy leading edge is presented at a Reynolds number of 3X106. The flow is resolved by considering the RANS (Reynolds Average Navier-Stokes) equations. The baseline geometry is based on th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bffd2476367731f0d613a19433e49704
http://www.scielo.org.co/scielo.php?script=sci_arttext&pid=S0120-62302021000100069&lng=en&tlng=en
http://www.scielo.org.co/scielo.php?script=sci_arttext&pid=S0120-62302021000100069&lng=en&tlng=en
Autor:
Adson Agrico de Paula
Publikováno v:
Biblioteca Digital de Teses e Dissertações da USPUniversidade de São PauloUSP.
Recently, the wavy leading edge airfoils, inspired by the humpback whale´s flipper, have been investigated, as flow control mechanisms, at low Reynolds numbers in order to improve aerodynamic performance in this particular flow regime. The overall a
Publikováno v:
16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
From the start of aviation, designers have been searching for methods and technologies to reduce the required fuel burn of commercial aircraft. Wingtip devices in special winglets offer a way of significant drag reduction for transport airplanes. Win
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d735318ffd3a35ed660cd74b8bfacbf1
https://doi.org/10.2514/6.2015-3437
https://doi.org/10.2514/6.2015-3437
Autor:
Julio Romano Meneghini, Roberto G. da Silva, Bruno Ricardo Massucatto Padilha, Bento Silva de Mattos, Adson Agrico de Paula
Publikováno v:
23rd ABCM International Congress of Mechanical Engineering.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a20b73a4126f3c8cc889980f747bbea0
https://doi.org/10.20906/cps/cob-2015-1699
https://doi.org/10.20906/cps/cob-2015-1699
Autor:
Pires Fonseca, William Denner1 fonsecawdp@gmail.com, Rosario Da Silva, Rafael1, Marcondes Orselli, Reinaldo2, Agrico de Paula, Adson3, da Silva, Ricardo Galdino4
Publikováno v:
Revista Facultad de Ingeniería Universidad de Antioquia. Jan-Mar2021, Issue 98, p69-77. 9p.
Publikováno v:
Applied Sciences (2076-3417); Feb2023, Vol. 13 Issue 3, p1425, 231p
Modeling wind turbine blades by geometrically-exact beam and shell elements: a comparative approach.
Autor:
Celso Jaco Faccio Júnior
Publikováno v:
Biblioteca Digital de Teses e Dissertações da USPUniversidade de São PauloUSP.
The total wind power capacity installed in the world has substantially grown during the last few years, mainly due to the increasing number of horizontal axis wind turbines (HAWT). Consequently, a big effort was employed to increase HAWT\'s power cap
Autor:
Celso Jaco Faccio Júnior
Publikováno v:
Biblioteca Digital de Teses e Dissertações da USP
Universidade de São Paulo (USP)
instacron:USP
Universidade de São Paulo (USP)
instacron:USP
The total wind power capacity installed in the world has substantially grown during the last few years, mainly due to the increasing number of horizontal axis wind turbines (HAWT). Consequently, a big effort was employed to increase HAWT\'s power cap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2f8d754eeb23445e914548034a9d5b84
Autor:
Edgard Kheit Takara
Publikováno v:
Biblioteca Digital de Teses e Dissertações do ITAInstituto Tecnológico de AeronáuticaITA.
O objetivo do trabalho é elaborar e validar um código computacional para a determinação da Polar de Arrasto classe 2 de aeronaves que produza resultados com a melhor aproximação possível com a realidade para a utilização durante a fase de an