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CORDIS - Resultados de investigaciones de la UE
CORDIS

Medium-range hybrid low-pollution flexi-fuel/hydrogen sustainable engine

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

Data Management Plan (se abrirá en una nueva ventana)

Task 11 The DMP will provide the identification elements and the descriptions of the data sets and will include details regarding how the research data will be handled during theproject and how they will be preserved after it is completed Success indicator complete documentation ready and approved by the governing bodies of the project in agreement with the PO

Data Management Plan Update 1 (se abrirá en una nueva ventana)

Task 1.2: Update of the Data Management Plan n.1 is released. Success indicator: report timely issued.

Project Handbook (se abrirá en una nueva ventana)

Task 11 The Project Handbook brings together a wide range of general operational information including contact details roles and responsibilities of the partners according to the governance structure operational and reporting processes templates procedures for the preparation of deliverables Success indicator complete documentation ready and approved by the governing bodies of the project in agreement with the PO

Dissemination and Exploitation Plan (se abrirá en una nueva ventana)

Task 1.3: The D&E plan will provide the details of Communication, Dissemination and Exploitation of the results. It will also contain the relevant KPIs established by the project governing bodies in agreement with the PO. Success indicator: complete documentation ready and approved by the governing bodies of the project in agreement with the PO.

Dissemination and Exploitation Plan Update1 (se abrirá en una nueva ventana)

Task 1.3: Update of the Dissemination and Communication Report n.1 is released. Success indicator: report timely issued.

Fuel selection report (se abrirá en una nueva ventana)

Task 6.2: Conventional fossil jet fuels as well as a range of sustainable jet fuels with a range of specifications covering a range of Cetane numbers between 17 and 80 will be selected and acquired. This range of jet fuels should include JetA1, JP5 and dodecane together, with a few low and high Cetane number (sustainable) jet fuels. Success indicator: fuels are documented and acquisition is successfully accomplished and documented.

Description of baseline combustor set- up (se abrirá en una nueva ventana)

Task 6.1: A brief description of the combustor model to be used for experiments in WP6, numerical simulations in WP3 and hidden physics extraction in WP4 is isued. Success indicator: complete documentation is issued.

Reduced mechanism for SAF- blends (se abrirá en una nueva ventana)

Task 2.1: The surrogate model and reduced mechanism for SAF blends and engine’s Chemical Reactor Network model for evaluation of pollutant emissions in conceptual design stage is use-ready. Success indicator: successful validation of reduced mechanism against detailed mechanism in laminar flames (premixed/non-premixed); Reaction-Network framework validated numerically against steady-state simulations of standard combustor design.

Chemistry-turbulence interaction model (se abrirá en una nueva ventana)

Task 3.1: An experimentally validated improved turbulence-chemistry interaction model for variable fuel blends is delivered specifically for the efficiency-driven needs of scale-resolving simulations on Tier-0 HP-Clusters. Success indicator: improved speed-up and scalability (>5%) of computations in a canonic jet-flame configuration.

Minimal-fidelity model of reference engine (se abrirá en una nueva ventana)

Task 23 Based on an available research engine configuration a small twinspool turbofan provided by the partnerLUND a first airframeengine matching and minimalfidelity design will be carried out based essentially onperformance parameters using conventional JetA fuels Success indicator minimalfidelity model validated against lowfidelity numerical simulations of the same configuration

Minimal-fidelity model of airframe (se abrirá en una nueva ventana)

Task 2.2: Minimal-fidelity model of the selected airframe configuration and selection of mission conditions for a typical short-range flight is delivered. Sucess indicator: minimal fidelity model validated on the basis of existing data and procedures (e.g. JTI project).

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