inveSTigation of an ultrA compact Reverse flow combusTor

Información del proyecto

START

Identificador del acuerdo de subvención: 785217

DOI

10.3030/785217

Proyecto cerrado

Fecha de la firma de la CE 24 Enero 2018

Fecha de inicio 1 Febrero 2018

Fecha de finalización 31 Marzo 2021

Financiado con arreglo a

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coste total

€ 640 867,50

Aportación de la UE

€ 640 867,50

Coordinado por

UNIVERSITA DEGLI STUDI DI FIRENZE
Italy

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Documents, reports (4)

Plan for Communication, Dissemination and Exploitation of project results

This document will contain the plan of communication activities, a plan for dissemination of project results and a plan for exploitation of project results and handling of IP rights linked to project outputs

Test specification

A report describing the detailed specification of full annular tests execution. This document will represent the operative instructions for the test campaign. The document will be issued by COSVIG but it will include contribution also from the Topic Manager

Report on Communication, Dissemination and Exploitation actions

This document will report on the actual communication and dissemination activities of project results and a summary of the exploitation of project results and handling of IP rights linked to project outputs.

Innovative numerical models description

This report will describe in details the numerical modelling strategies adopted in the final release of the innovative uTherm3D approach.

Publicaciones

Peer reviewed articles (2)

Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD

Autores: Davide Bertini, Lorenzo Mazzei and Antonio Andreini
Publicado en: Entropy, 2021, ISSN 1099-4300
Editor: Multidisciplinary Digital Publishing Institute (MDPI)

Large-Eddy Simulation of a Model Aero-Engine Sooting Flame With a Multiphysics Approach

Autores: Simone Paccati, Davide Bertini, Lorenzo Mazzei, Stefano Puggelli, Antonio Andreini
Publicado en: Flow, Turbulence and Combustion, 2020, ISSN 1386-6184
Editor: Kluwer Academic Publishers
DOI: 10.1007/s10494-020-00202-5

Conference proceedings (2)

Multiphysics Numerical Investigation of an Aeronautical Lean Burn Combustor

Autores: D. Bertini, L. Mazzei, A. Andreini, B. Facchini
Publicado en: Volume 5B: Heat Transfer, Edición ASME Turbo Expo 2019 - GT2019-91437, 2019, ISBN 978-0-7918-5865-3
Editor: American Society of Mechanical Engineers
DOI: 10.1115/gt2019-91437

LARGE-EDDY SIMULATION OF A MODEL AERO-ENGINE SOOTING FLAME WITH A MULTIPHYSICS APPROACH

Autores: S. Paccati, D. Bertini, L. Mazzei, A. Andreini and S. Puggelli
Publicado en: Mediterrean Combustion Symposium 2019 - MCS11, 2019
Editor: Combustion Institute