Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Stefano Caloni"'
Publikováno v:
Aerospace, Vol 5, Iss 4, p 116 (2018)
The turbine tip geometry can significantly alter the performance of the turbine stage; its design represents a challenge for a variety of reasons. Multiple disciplines are involved in its design and their requirements limit the creativity of the desi
Externí odkaz:
https://doaj.org/article/2543041592f044e9a559ca79af2afc27
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 230:709-720
The over-tip leakage represents a third of the loss encountered in a typical high-pressure turbine stage. In this paper, numerical investigations are carried out to study the effects of different tip designs on the aerodynamic performance and cooling
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5284fe22a2b195005d345eea77af87e6
https://doi.org/10.1177/0957650916661459
https://doi.org/10.1177/0957650916661459
Autor:
Shahrokh Shahpar, Stefano Caloni
Publikováno v:
Volume 5A: Heat Transfer.
The design of a high pressure turbine blade is a challenging task requiring multiple disciplines to be solved simultaneously. Most recently, conjugate analyses are being developed to tackle such a problem; they are able to resolve both the fluid dyna
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::641ff00df48cb038a10f60de1e906877
https://doi.org/10.1115/gt2016-57794
https://doi.org/10.1115/gt2016-57794
Autor:
Stefano Caloni, Shahrokh Shahpar
Publikováno v:
Volume 5A: Heat Transfer.
In this paper the aero-thermal performance of a high pressure turbine rotor blade is investigated, making use of coupled and uncoupled simulations. The fluid domain is solved via Finite Volume analyses whilst Finite Elements are used in the solid dom
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e748c3968cda3607aeb96ec6551db19
https://doi.org/10.1115/gt2015-43292
https://doi.org/10.1115/gt2015-43292
Publikováno v:
Volume 2C: Turbomachinery.
This paper presents a novel optimisation methodology based on both Adjoint sensitivity analysis and trust-based dynamic response surface modelling to improve performance of a modern turbine of a large civil aero-engine in the presence of high-fidelit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::eff09df28d02a8761745013141344daf
https://doi.org/10.1115/gt2014-26628
https://doi.org/10.1115/gt2014-26628
Autor:
Stefano Caloni, Shahrokh Shahpar
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 135
Modern lean-burn combustors make use of high flow swirl to maintain flame stability. The swirling flow can persist downstream of the turbine first vane, changing the loading on the rotor, leading to a reduction in efficiency. This paper presents the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::61720ca6a7a4402c758f873b7a1eb0ab
https://doi.org/10.1115/1.4007977
https://doi.org/10.1115/1.4007977
Autor:
Shahrokh Shahpar, Stefano Caloni
Publikováno v:
Volume 8: Turbomachinery, Parts A, B, and C.
Modern lean-burn combustors make use of high flow swirl to maintain flame stability. The swirling flow can persist downstream of the turbine first vane, changing the loading on the rotor, leading to a reduction in efficiency. This paper presents the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5810072466cbad100afb1f8a3d9d131
https://doi.org/10.1115/gt2012-69228
https://doi.org/10.1115/gt2012-69228