Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Andre Mignosi"'
Publikováno v:
Flow, Turbulence and Combustion (formerly Applied Scientific Research). 71:221-245
In transonic flow conditions, the shock wave/turbulent boundary layer interaction and the flow separations on the upper wing surfaces of civil aircraft induce flow instabilities, ‘buffet’ and then structural vibrations, ‘buffeting’. Buffeting
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00f6d767545b83a608ba9582809d0340
https://doi.org/10.1023/b:appl.0000014918.93432.4f
https://doi.org/10.1023/b:appl.0000014918.93432.4f
Publikováno v:
ICIASF 2005 RecordInternational Congress onInstrumentation in AerospaceSimulation Facilities.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::20dbb9bebe8dc0754bb207a83426b01e
https://doi.org/10.1109/iciasf.2005.1569932
https://doi.org/10.1109/iciasf.2005.1569932
Publikováno v:
21st AIAA Applied Aerodynamics Conference.
In transonic flow conditions, the shock wave / turbulent boundary layer interaction and flow separations, which induce flow instabilities, “buffet”, and then structure vibrations, “buffeting”, can have an important influence on the aerodynami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::305d448fc54b493089d97577d1051e9b
https://doi.org/10.2514/6.2003-3667
https://doi.org/10.2514/6.2003-3667
Publikováno v:
ICIASF 2001 Record, 19th International Congress on Instrumentation in Aerospace Simulation Facilities (Cat. No.01CH37215).
A Doppler Global Velocimetry System (DGV) has been developed and qualified at ONERA. It can perform planar three component mean velocity measurements in air flows. Our system was designed with special regards to wind tunnel applications. The technica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e70f50431458985e4e0615aa1da1868b
https://doi.org/10.1109/iciasf.2001.960252
https://doi.org/10.1109/iciasf.2001.960252
Publikováno v:
ICIASF 2001 Record, 19th International Congress on Instrumentation in Aerospace Simulation Facilities (Cat. No.01CH37215).
In transonic flow conditions, the shock wave/turbulent boundary layer interaction and flow separations, which induce flow instabilities, "buffet", and then structure vibrations, "buffeting", can have an important influence on the aerodynamic behavior
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f20330e9071bd992c81241a9c8e2a386
https://doi.org/10.1109/iciasf.2001.960274
https://doi.org/10.1109/iciasf.2001.960274
Publikováno v:
Fluids 2000 Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1ad1b91918cf05d9d8c99aaa18b6cbb
https://doi.org/10.2514/6.2000-2609
https://doi.org/10.2514/6.2000-2609
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