Zobrazeno 1 - 6
of 6
pro vyhledávání: '"J. Woisetschla¨ger"'
Publikováno v:
Journal of Turbomachinery. 126:297-305
The current paper presents steady and unsteady flow data of a transonic test turbine stage operating under flow conditions similar to modern highly loaded gas turbines. Measurements were performed between stator and rotor as well as downstream of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b98e45b7ca520de16fad2bc39af77162
https://doi.org/10.1115/1.1649745
https://doi.org/10.1115/1.1649745
Autor:
Oliver Schennach, Rene Pecnik, Berardo Paradiso, Giacomo Persico, J. Woisetschla¨ger, Paolo Gaetani
Publikováno v:
Volume 6: Turbomachinery, Parts A, B, and C.
The unsteady and fully three-dimensional aerodynamics of HP turbines represent a relevant research branch for future aero-engine design. When stator-rotor interaction mechanisms and clocking effects are of concern, advanced measurement techniques as
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9861384188a37ebc8c8b1206d944e7f8
https://doi.org/10.1115/gt2008-50291
https://doi.org/10.1115/gt2008-50291
Publikováno v:
Volume 6: Turbomachinery, Parts A and B.
The current paper presents experimental clocking investigations of the flow field in midspan in a high-pressure transonic turbine with a downstream vane row (1.5 stage machine). Laser-Doppler-Velocimetry measurements were carried out in order to reco
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3146374835397004d2c1e7ae236010fd
https://doi.org/10.1115/gt2006-90264
https://doi.org/10.1115/gt2006-90264
Autor:
L. Innocenti, Wolfgang Sanz, E. Go¨ttlich, J. Woisetschla¨ger, Herbert Jericha, Andrea Vacca, E. Rossi, Bruno Facchini
Publikováno v:
Scopus-Elsevier
Gas turbine design technology requires the development of transonic turbine stages capable of carrying high stage load and of handling hot gas temperatures at turbine inlet. A reliable cooling system is necessary to cope with shocks emanating from pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ccb2d9f302326af5cbba76faf374ef67
https://doi.org/10.1115/gt2004-53712
https://doi.org/10.1115/gt2004-53712
Publikováno v:
Volume 6: Turbo Expo 2003, Parts A and B.
The current paper presents steady and unsteady flow data of a transonic test turbine stage operating under flow conditions similar to modern highly loaded gas turbines. Measurements were performed between stator and rotor as well as downstream of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e01e6e011abebe612f34e5fab6853c33
https://doi.org/10.1115/gt2003-38266
https://doi.org/10.1115/gt2003-38266
Publikováno v:
Volume 5: Turbo Expo 2002, Parts A and B.
Gas turbine design technology requires the development of transonic turbine stages capable of carrying high stage load and of handling hot gas temperatures at turbine inlet. A reliable cooling system is necessary to cope with the shock system in the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22b19674966d291690d1ff779bd714a6
https://doi.org/10.1115/gt2002-30341
https://doi.org/10.1115/gt2002-30341