Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Diego Benito"'
Publikováno v:
CLEI Electronic Journal, Vol 27, Iss 2 (2024)
the concept of digital transformation involves exploiting digital technologies to generate new ways of doing things in organizations, including the creation of new processes, models, and services that produce value based on the digitization of data a
Externí odkaz:
https://doaj.org/article/6cd3f379f11b488cac0bdfe1880a88fe
Autor:
Abdolkarim Sheikhansari, Ben Shaw, Jonathan N. Knapton, Ehsan Alborzi, Diego Benito, Simon Blakey
Publikováno v:
Tribology Transactions. 64:381-391
A test apparatus is described that evaluates the performance of static aviation seals under an environment similar to the lubrication system in gas turbine engines. The seals can be tested at opera...
Autor:
Cayo Alcos, Diego Benito
Publikováno v:
Repositorio de Tesis - UNMSMUniversidad Nacional Mayor de San Marcos.
Propone el desarrollo de un E-Health Cloud describiendo el análisis de procesos, identificación de requerimientos de software, diseño de wireframes, comunicación de componentes, infraestructura, estrategia de pruebas y despliegue en la nube. El E
Externí odkaz:
http://cybertesis.unmsm.edu.pe/handle/cybertesis/7913
Autor:
Andy J. Keane, Norbert Kill, Jeffery A. Dixon, David J. J. Toal, Trevor T. Robinson, Jingbin Yang, Matthew Price, Diego Benito, Alain Remouchamps
Publikováno v:
Toal, D J J, Keane, A J, Benito, D, Dixon, J A, Yang, J, Price, M, Robinson, T, Remouchamps, A & Kill, N 2014, ' Multi-Fidelity Multidisciplinary Whole Engine Thermo-Mechanical Design Optimization ', Journal of Propulsion and Power, vol. 30, no. 6, pp. 1654-1666 . https://doi.org/10.2514/1.B35128
Traditionally, the optimization of a turbomachinery engine casing for tip clearance has involved either two-dimensional transient thermomechanical simulations or three-dimensional mechanical simulations. This paper illustrates that three-dimensional
Publikováno v:
Volume 4: Heat Transfer, Parts A and B.
This paper presents a 3D thermo-mechanical modelling method to calculate compressor local tip running clearances. The method requires a solid geometry representation of the compressor casings and main engine structures, including local geometry featu