inveSTigation of an ultrA compact Reverse flow combusTor

Project Information

START

Grant agreement ID: 785217

DOI 10.3030/785217

Project closed

EC signature date 24 January 2018

Start date 1 February 2018

End date 31 March 2021

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost € 640 867,50

EU contribution € 640 867,50

Coordinated by

UNIVERSITA DEGLI STUDI DI FIRENZE
Italy

Deliverables

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.

Publications

Peer reviewed articles (2)

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

Author(s): Davide Bertini, Lorenzo Mazzei and Antonio Andreini
Published in: Entropy, 2021, ISSN 1099-4300
Publisher: Multidisciplinary Digital Publishing Institute (MDPI)

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

Author(s): Simone Paccati, Davide Bertini, Lorenzo Mazzei, Stefano Puggelli, Antonio Andreini
Published in: Flow, Turbulence and Combustion, 2020, ISSN 1386-6184
Publisher: Kluwer Academic Publishers
DOI: 10.1007/s10494-020-00202-5

Conference proceedings (2)

Multiphysics Numerical Investigation of an Aeronautical Lean Burn Combustor

Author(s): D. Bertini, L. Mazzei, A. Andreini, B. Facchini
Published in: Volume 5B: Heat Transfer, Issue ASME Turbo Expo 2019 - GT2019-91437, 2019, ISBN 978-0-7918-5865-3
Publisher: American Society of Mechanical Engineers
DOI: 10.1115/gt2019-91437

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

Author(s): S. Paccati, D. Bertini, L. Mazzei, A. Andreini and S. Puggelli
Published in: Mediterrean Combustion Symposium 2019 - MCS11, 2019
Publisher: Combustion Institute