Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Jean-Pierre Archambaud"'
Publikováno v:
Scopus-Elsevier
Laminar-turbulent transition remains a critical issue in a number of cases, including drag reduction, performance prediction of high-lift systems, improved accuracy in general computational fluid dynamics, and reduction of computation cycles for deve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2c9d0c5b96209cad0ecacbbce5780a7d
https://doi.org/10.2514/1.42990
https://doi.org/10.2514/1.42990
Autor:
Onera Toulouse, Thomas Streit, Uwe Fey, Yasuhiro Egami, Ardeshir Hanifi, Jürgen Quest, Jean Perraud, Geza Schrauf, Raffaele Donelli, Jean-Pierre Archambaud
Publikováno v:
Scopus-Elsevier
With the goal of studying Natural Laminar Flow (NLF) wings for future ‘green’ transport aircraft, the aim of the European Research Project TELFONA is to develop and demonstrate the possibility of testing full aircraft models at large Reynolds num
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8e3e92682f280b55fd6eaa7d27a11335
https://elib.dlr.de/61758/
https://elib.dlr.de/61758/
Autor:
Ardeshir Hanifi, Uwe Fey, Stefan Hein, Jürgen Quest, Geza Schrauf, Raffaele Donelli, Thomas Streit, Yasuhiro Egami, Jean Perraud, Jean-Pierre Archambaud
Publikováno v:
Seventh IUTAM Symposium on Laminar-Turbulent Transition ISBN: 9789048137220
A wind–tunnel experiment on laminar-turbulent transition has been performed in ETW (the European Transonic Wind Tunnel in Koln) at high Reynolds number and cryogenic conditions. The studied geometry is a sting mounted full model in swept–wing con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::07f588c230f14cb14507b13084ffedff
https://doi.org/10.1007/978-90-481-3723-7_98
https://doi.org/10.1007/978-90-481-3723-7_98
Autor:
Jean-Luc Godard, Johann Valentin Krier, Raffaele Donelli, Jean-Pierre Archambaud, Daniel Arnal, Ardeshir Hanifi, Stefan Hein
Publikováno v:
Seventh IUTAM Symposium on Laminar-Turbulent Transition ISBN: 9789048137220
This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supersonic flow. The first part deals with the control of the transition due to crossflow (CF) instabilities present on a swept wing, by using Micron-Sized
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::133151139f77438d30eb6a9230f061c5
https://doi.org/10.1007/978-90-481-3723-7_10
https://doi.org/10.1007/978-90-481-3723-7_10
Publikováno v:
34th AIAA Fluid Dynamics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5891fb8a4288bdc33f7f9e6eff157f33
https://doi.org/10.2514/6.2004-2245
https://doi.org/10.2514/6.2004-2245