Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Bogdan C. Cernat"'
Autor:
Bogdan C. Cernat, Sergio Lavagnoli
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 4, Iss 2, p 12 (2019)
The present research focused on the analysis of the leakage flows developing from advanced blade tip geometries. The aerodynamic field of a contoured blade tip and of a high-performance rimmed blade were investigated against a baseline squealer rotor
Externí odkaz:
https://doaj.org/article/adf859445d68486cba953a105abb6140
Autor:
Sergio Lavagnoli, Bogdan C. Cernat
While modern engine manufacturers devote significant efforts to the development of reliable and efficient machines, the introduction of novel, optimized components in the hot gas path represents a risky opportunity. Accurate experimental and numerica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fb6b1cc5e7b2d17ef9f38f10182d7aa7
https://doi.org/10.1115/1.0002984v
https://doi.org/10.1115/1.0002984v
Publikováno v:
Journal of Turbomachinery. 141
The leakage flows within the gap between the tips of unshrouded rotor blades and the stationary casing of high-speed turbines are the source of significant aerodynamic losses and thermal stresses. In the pursuit for higher component performance and r
Publikováno v:
2018 Joint Propulsion Conference.
Publikováno v:
Volume 5B: Heat Transfer.
The leakage flows within the gap between the tips of unshrouded rotor blades and the stationary casing of high-speed turbines are the source of significant aerodynamic losses and thermal stresses. In the pursuit for higher component performance and r
Publikováno v:
Volume 5B: Heat Transfer.
This paper presents two examples of temperature and heat transfer measurements performed in different setups, both being representative cases of internal cooling cavities. In this investigation, Thermochromic Liquid Crystals (TLCs) were applied on th
Publikováno v:
Volume 5B: Heat Transfer.
Blade tip design and tip leakage flows are crucial aspects for the development of modern aero-engines. The inevitable clearance between stationary and rotating parts in turbine stages generates high-enthalpy unsteady leakage flows that strongly reduc
Publikováno v:
Journal of Heat Transfer. 140
The detailed flow field and heat transfer were experimentally investigated in a channel with a circular cross section and equipped with a helical rib of low blockage ratio. Stereoscopic particle image velocimetry (S-PIV) was applied in order to measu
Publikováno v:
Volume 5B: Heat Transfer.
The detailed flow field and heat transfer were experimentally investigated in a channel with a circular cross section and equipped with a helical rib of low blockage ratio. Stereoscopic Particle Image Velocimetry (S-PIV) was applied in order to measu