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DEMOS SIGNED

Developing advanced Engine Multi-disciplinary Optimization Simulations (DEMOS)

Total Cost €

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EC-Contrib. €

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Partnership

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Project "DEMOS" data sheet

The following table provides information about the project.

Coordinator
EMPRESARIOS AGRUPADOS INTERNACIONAL SA 

Organization address
address: CALLE MAGALLANES 3
city: MADRID
postcode: 28015
website: www.empre.es

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Spain [ES]
 Project website https://www.ecosimpro.com/demos/
 Total cost 410˙450 €
 EC max contribution 410˙450 € (100%)
 Programme 1. H2020-EU.3.4.5.4. (ITD Airframe)
 Code Call H2020-CS2-CFP01-2014-01
 Funding Scheme CS2-RIA
 Starting year 2016
 Duration (year-month-day) from 2016-01-01   to  2019-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    EMPRESARIOS AGRUPADOS INTERNACIONAL SA ES (MADRID) coordinator 110˙000.00
2    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 160˙787.00
3    NATIONAL TECHNICAL UNIVERSITY OF ATHENS - NTUA EL (ATHINA) participant 139˙662.00

Map

 Project objective

The “Innovative Aircraft Architecture” technology stream of the Clean Sky 2 Airframe ITD focuses on advanced power-plant solutions (such as CROR and UHBR) that are able to deliver a significant gain in aircraft performance. Project DEMOS will develop advanced predictive modelling and simulation capabilities for engine design space exploration and performance optimization of such novel propulsion systems. The overall and detailed objectives of Project DEMOS may be summed up as follows: • Assess, adapt and further develop a set of reliable and robust models to simulate/optimise performance of UHBR propulsion system architectures • Identify, build and integrate simulation models of specific (novel) components which may be considered as enablers of the technology • Demonstrate and assess the effect and influence of these components on the propulsion system performance in terms of overall performance, increase in mass, effect on lifing characteristics of the propulsion system and on the operating/ maintenance cost • Develop a modular approach to enable integration and further development of main modules/models for preliminary design process • Facilitate complex integration requirements • Improve process efficiency through the development of advanced solvers and adequate numerical methods to address complex system simulations • Development of advanced simulation techniques to improve the monitoring of communication between integrated models, robustness and convergence • Enable complex propulsion system performance optimisation with constraint handling capability • Develop a suite of advanced solvers to enable extended transient capabilities and simulation of complex systems transients and control The project will build on the established multi-disciplinary concept design tools and further develop and adapt them in terms of applicability to advanced technologies and multi-objective concept analysis and selection.

 Publications

year authors and title journal last update
List of publications.
2019 Alexios Alexiou; Nikolaos Aretakis; Dimitrios Kapsoulis; Konstantinos Mathioudakis; Kyriakos Giannakoglou
Multidisciplinary Preliminary Aero-Engine Design for More Sustainable Flight Missions
published pages: , ISSN: , DOI: 10.5281/zenodo.3737936
2020-04-23
2017 Alexios Alexiou; Nikolaos Aretakis; Ioannis Roumeliotis; Ioannis Kolias; Konstantinos Mathioudakis
Performance modelling of an ultra-high bypass ratio geared turbofan
published pages: , ISSN: , DOI: 10.5281/zenodo.3737870
2020-04-23

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The information about "DEMOS" are provided by the European Opendata Portal: CORDIS opendata.

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