Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Jean-Pierre Rosenblum"'
Autor:
Andreea BOBONEA, Florin MUNTEANU, Jean-Pierre ROSENBLUM, Catalin NAE, Corneliu STOICA, Mihai Victor PRICOP, Ionut BRINZA
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 67-75 (2012)
This paper presents experimental results obtained with passive high lift systems using a combination of smart flap kinematics and vortex generators. A mid-scale 2.5D wind tunnel model based on DLR-F15 is tested in INCAS Subsonic Wind Tunnel, swept at
Externí odkaz:
https://doaj.org/article/c14e13e8a6fb47f995f084903d9c9c13
Autor:
Pierluigi Iannelli, Jochen Wild, Shia-Hui Peng, Vlad Ciobaca, Petr Vrchota, Stefan Wallin, Michel Costes, Jean-Pierre Rosenblum, Ales Prachar, Peter Eliasson, Jean-Luc Hantrais-Gervois
Publikováno v:
CEAS Aeronautical Journal
CEAS Aeronautical Journal, Springer, 2019, ⟨10.1007/s13272-019-00402-4⟩
CEAS Aeronautical Journal, Springer, 2019, ⟨10.1007/s13272-019-00402-4⟩
International audience; Within the European project AFLoNext, one of the technological streams is dedicated to the investigation of active flow control (AFC) to increase the robustness of the wing tip design at takeoff conditions, whilst allowing the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bc3480de3ae30013b40686d48e3bfa8b
https://hal.archives-ouvertes.fr/hal-02614009
https://hal.archives-ouvertes.fr/hal-02614009
Autor:
Elie Carafoli, Ionut Brinza, Catalin Nae, Jean-Pierre Rosenblum, Florin Munteanu, Corneliu Stoica, Mihai Victor Pricop, Quai Marcel Dassault, Andreea Bobonea, B-dul Iuliu Maniu
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 67-75 (2012)
This paper presents experimental results obtained with passive high lift systems using a combination of smart flap kinematics and vortex generators. A mid-scale 2.5D wind tunnel model based on DLR-F15 is tested in INCAS Subsonic Wind Tunnel, swept at
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::be561869787263292f12fd9c03bbda79
http://bulletin.incas.ro/files/pricop_stoica_nae_munteanu_rosenblum_bobonea_brinz.pdf
http://bulletin.incas.ro/files/pricop_stoica_nae_munteanu_rosenblum_bobonea_brinz.pdf
Publikováno v:
Comptes Rendus Mécanique. 333:810-817
Resume En ecoulement transsonique, l'interaction onde de choc/couche limite turbulente et les decollements qui en decoulent sur l'extrados d'une aile induisent des instabilites appelees tremblement et provoquent des vibrations de la structure. Ce phe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::208ef130362a7de824825216ce1f222a
https://doi.org/10.1016/j.crme.2005.09.007
https://doi.org/10.1016/j.crme.2005.09.007
Publikováno v:
International Journal for Numerical Methods in Fluids. 49:171-182
In transonic flow conditions, the shock wave/turbulent boundary layer interaction and flow separations on wing upper surface induce flow instabilities, ‘buffet’, and then the buffeting (structure vibrations). This phenomenon can greatly influence
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3c29537ae3a88af23cd9f7118565f706
https://doi.org/10.1002/fld.991
https://doi.org/10.1002/fld.991
Publikováno v:
25th AIAA Applied Aerodynamics Conference.
T he paper will first describe the challenges associated to the aerodynamic design of UCAV afterbodies. The issues of turbulence modeling to capture complex flow features relative to stealthy afterbody shapes will also be addressed. The development p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e16233d5ef5b0cd2ba9ef89a90336f28
https://doi.org/10.2514/6.2007-4570
https://doi.org/10.2514/6.2007-4570
Publikováno v:
Volume 2: Fora.
The control of subsonic high lift induced separation on airfoil may improve the flight envelope of current aircraft or even simplify the complex and heavy high-lift devices on commercial airframes. Until now, synthetic jets have proved a really inter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc7f9da682a56f419c5b29106477b86f
https://doi.org/10.1115/fedsm2006-98540
https://doi.org/10.1115/fedsm2006-98540