Zobrazeno 1 - 10
of 69
pro vyhledávání: '"Tiziano Ghisu"'
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:
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
Publikováno v:
Renewable Energy. 197:583-593
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
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
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
Publikováno v:
Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery.
The term uncertainty quantification (UQ) refers to a set of techniques which are used to measure the statistical variability of several input parameters. In recent years, UQ has become increasingly relevant due to its applications in robust design an
Publikováno v:
AIAA AVIATION 2021 FORUM
Regression-based Polynomial Chaos expansions offer several advantages over projection-based approaches, including their lower computation cost and greater flexibility. In the presence of expensive function evaluations, such as with computational flui
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2a874a8cdf4cf4a2cc38bfd38b1e376f
https://zenodo.org/record/5907398
https://zenodo.org/record/5907398