Belmar Gil, Mario(Universitat Politècnica de València, 2021-01-21)
[ES] El principal desafío en los motores turbina de gas empleados en aviación reside en aumentar la eficiencia del ciclo termodinámico manteniendo las emisiones contaminantes por debajo de las rigurosas restricciones. Ésto ...
[ES] El principal objetivo de este trabajo es diseñar un ala para una aeronave de la que se conocen las especificaciones iniciales y comprobar mediante un análisis CFD que produce las prestaciones necesarias para mantener ...
Belmar Gil, Mario(Universitat Politècnica de València, 2018-10-17)
El presente Trabajo Fin de Master trata la resolución numérica mediante códigos CFD de una novedosa estrategia de inyección/combustión, conocida como Lean Direct Injection, aplicada a los motores de flujo continuo. Este ...
[EN] Lean Direct Injection (LDI) emerged as an interesting concept to limit NOx emissions in aero engines at the cost of operating close to the flame lean blow-off limit. In this technology, fuel is injected into a swirled ...
[EN] This work is focused on the numerical study of low-order coherent structures of a high-swirled laboratory-scaled combustor operated by a Lean Premixed (LP) injection system in non-reacting conditions through different ...
[EN] Fuel efficiency improvement and harmful emissions reduction are the main motivations for the development of gas turbine combustors. Numerical computational fluid dynamics (CFD) simulations of these devices are usually ...
[EN] The main challenge of next-generation aeronautical gas turbine engines lies in the increase of the efficiency of the cycle and the reduction of pollutant emissions below stringent restrictions. This has led to the ...
Payri, Raul; Salvador, Francisco Javier; Carreres, Marcos; Belmar-Gil, Mario(Elsevier, 2020-01-15)
[EN] In this paper, a one-dimensional computational model of the flow in a common-rail injector is used to compute local variations of fuel temperature (including the temperature change produced upon expansion across the ...