Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Victor Moënne-Loccoz"'
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 5, Iss 1, p 2 (2020)
The flow in the vaned diffuser of an aeronautical centrifugal compressor designed by Safran Helicopter Engines is analyzed through steady and unsteady pressure measurements at different rotation speeds. The analysis leads to the identification of dif
Externí odkaz:
https://doaj.org/article/d29be69821d44d11adbf3d9cf85ec35a
Publikováno v:
Volume 2B: Turbomachinery.
A boundary layer suction strategy is tested in a centrifugal compressor stage designed and built by Safran Helicopter Engines. According to previous numerical results, suction slots are disposed in the radial diffuser at the hub and the shroud near t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e18beafe548d340653637d8e02fafc5
https://doi.org/10.1115/gt2018-75365
https://doi.org/10.1115/gt2018-75365
Autor:
Victor Moënne-Loccoz, Pierre Laucher, Sébastien Goguey, Benoit Paoletti, Emmanuel Benichou, Isabelle Trébinjac
Publikováno v:
Journal of Thermal Science
Journal of Thermal Science, Springer Verlag (Germany), 2017, 26, pp.289-296. ⟨10.1007/s11630-017-0941-8⟩
Journal of Thermal Science, Springer Verlag (Germany), 2017, 26, pp.289-296. ⟨10.1007/s11630-017-0941-8⟩
The present paper gives the experimental results obtained in a centrifugal compressor stage designed and built by SAFRAN Helicopter Engines. The compressor is composed of inlet guide vanes, a backswept splittered unshrouded impeller, a splittered van
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ff42d78e1cfa2b4199ad7f0e95003bec
https://hal.archives-ouvertes.fr/hal-01724945
https://hal.archives-ouvertes.fr/hal-01724945
Publikováno v:
Mechanics & Industry
Mechanics & Industry, EDP Sciences, 2019, 20 (8), pp.805. ⟨10.1051/meca/2020026⟩
Mechanics & Industry, EDP Sciences, 2019, 20 (8), pp.805. ⟨10.1051/meca/2020026⟩
International audience; The present paper aims at providing an experimental analysis of the path to surge of a centrifugal compressor stage designed and built by Safran Helicopter Engines. Depending on the rotation speed of the compressor, two distin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4c21865169d09450f880195d3f72641c
https://doi.org/10.1051/meca/2020026
https://doi.org/10.1051/meca/2020026