Zobrazeno 1 - 10
of 97
pro vyhledávání: '"Tiziano Ghisu"'
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Publikováno v:
Aerospace, Vol 11, Iss 9, p 750 (2024)
As turbine entry temperatures of modern jet engines continue to increase, additional thermal stresses are introduced onto the high-pressure turbine rotors, which are already burdened by substantial levels of centrifugal and gas loads. Usually, for mo
Externí odkaz:
https://doaj.org/article/0a45e9aa7cf34bf78ffee33f58515629
Publikováno v:
Ocean Engineering. 206:107016
This reply is based on the discussion by Ghisu and Cambuli. With great interest, the authors have read the comments made by Ghisu and Cambuli. The comments severely criticizes our methodology and results, which actually provide us with fortunate oppo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5663ecefa2355ed609ee7e71cb25a528
https://doi.org/10.1016/j.oceaneng.2020.107016
https://doi.org/10.1016/j.oceaneng.2020.107016
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 8, Iss 3, p 24 (2023)
Due to the increasingly high turbine inlet temperatures, heat transfer analysis is now, more than ever, a vital part of the design and optimization of high-pressure turbine rotor blades of a modern jet engine. The present study aimed to find out how
Externí odkaz:
https://doaj.org/article/53b2d046d9c24004b56cc271af2cecc1
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 8, Iss 3, p 21 (2023)
An experimental investigation of the local flow field in a Wells turbine has been conducted, in order to produce a detailed analysis of the aerodynamic characteristics of the rotor and support the search for optimized solutions. The measurements were
Externí odkaz:
https://doaj.org/article/a52842b41c844ff79d35a24a87a95fec
Publikováno v:
Heat Transfer Engineering. :1-20
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::172e44c449050cf9a3efc5fe716923ff
https://doi.org/10.1080/01457632.2022.2134075
https://doi.org/10.1080/01457632.2022.2134075
Publikováno v:
Renewable Energy. 197:583-593
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3d0c04e669400f740f4768262ed0099
https://doi.org/10.1016/j.renene.2022.07.116
https://doi.org/10.1016/j.renene.2022.07.116
Publikováno v:
Journal of Turbomachinery. 144
The tip clearance size has historically been considered to be the main factor affecting stability range in axial fan and compressors. This paper reveals that the stall characteristics are defined by the axial momentum flux of the tip leakage flow and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6212f71cac7769ba875d29a7f9053425
https://doi.org/10.1115/1.4055350
https://doi.org/10.1115/1.4055350
Publikováno v:
Journal of Turbomachinery. 144
In-service deterioration can lead to undesired shape variations on high-pressure turbine rotor blades. This can have a significant impact on efficiency, power generation, and component life. Loss of power production from the high-pressure turbine rot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed949e7a28597e7ea9469bf6fcc423e4
https://doi.org/10.1115/1.4055267
https://doi.org/10.1115/1.4055267
Publikováno v:
Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics.
In-service deterioration can lead to undesired shape variations on high-pressure turbine rotor blades. This can have a significant impact on efficiency, power generation and component life. Loss of power production from the high-pressure turbine roto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f2290fe08bdae052387d78a00e114068
https://doi.org/10.1115/gt2022-82171
https://doi.org/10.1115/gt2022-82171