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25 projets européens trouvés

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 TERMINÉ 

Stability and Sensitivity Methods for Industrial Design (SSeMID)

Date du début: 1 janv. 2016, Date de fin: 31 déc. 2019,

The increasing environmental awareness of the European society has been always present in the aeronautical community, industry and research centres, having a definite influence on the way the aircraft of the future should be. In this line, the ACARE Vision for 2020, a Group of Renowned Personalities in the aeronautical field, has formulated a clear set of requirements for civil transport aircraft ...
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 10

 TERMINÉ 

Innovative Methodologies and technologies for reducing Aircraft noise Generation and Emission (IMAGE)

Date du début: 1 avr. 2016, Date de fin: 31 mars 2019,

The proposed project, IMAGE, is relevant to Topic MG-1.10-2015, aiming to enhance the EU-China collaborative effort focusing on “Innovative methods and numerical technologies for airframe and engine noise reduction”. The project consortium consists of 12 partners.The purpose of IMAGE is to investigate experimentally and numerically innovative airframe and engine noise-reduction technologies and, i ...
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 13

 TERMINÉ 

An Exascale Programming, Multi-objective Optimisation and Resilience Management Environment Based on Nested Recursive Parallelism (ALLScale)

Date du début: 1 oct. 2015, Date de fin: 30 sept. 2018,

Extreme scale HPC systems impose significant challenges for developers aiming at obtaining applications efficiently utilising all available resources. In particular, the development of such applications is accompanied by the complex and labour-intensive task of managing parallel control flows, data dependencies and underlying hardware resources – each of these obligations constituting challenging ...
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 7

 TERMINÉ 

Aeroelastic Gust Modelling (AEROGUST)

Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,

Encounters with atmospheric turbulence are a vitally important in the design and certification of many manmade structures such as aircraft and wind turbines. Gusts cause rapid changes in the flow about the structures which leads to rigid and flexible unsteady responses. Knowledge of aircraft/gust interactions is therefore vital for loads estimation during aircraft design as it impacts on control s ...
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 13

 TERMINÉ 

Towards Industrial LES/DNS in Aeronautics – Paving the Way for Future Accurate CFD (TILDA)

Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,

...essary to overcome the (still) existing lack in confidence in CFD usage, based on turbulence modelling. The TILDA project will offer methods and approaches combining advanced and efficient high-order numerical schemes (HOMs) with innovative approaches for LES and DNS in order to resolve all relevant flow features on tens of thousands of processors in order to get close to a full LES/DNS solution f ...
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 12

 TERMINÉ 

Computational Cloud Services and Workflows for Agile Engineering (CloudFlow)

Date du début: 1 juil. 2013, Date de fin: 31 déc. 2016,

Traditionally, the European manufacturing industry is characterized by innovative technology, quality processes and robust products which have leveraged Europe's industrialization. However, globalization has exposed Europe's industry to new emerging and industrialized manufacturing markets and the current economic challenges have decelerated the internal boost and investment, respectively. Hence, ...
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 29

 TERMINÉ 

Uncertainty Management for Robust Industrial Design in Aeronautics (UMRIDA)

Date du début: 1 oct. 2013, Date de fin: 30 sept. 2016,

...g conditions are a superposition of numerous uncertainties under which the industrial products operate (uncertainties on operational conditions, on geometries resulting from manufacturing tolerances, numerical error sources and uncertain physical model parameters). Major new developments in this new scientific area of Uncertainty Management and Quantification (UM and UQ) and Robust Design methods ...
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 22

 TERMINÉ 

new MAterials and REliability in offshore WINd Turbines technology (MARE-WINT)

Date du début: 1 oct. 2012, Date de fin: 30 sept. 2016,

One of the strategic objectives of the industrial initiative of the SET Plan on wind energy is to reduce cost of energy by improving reliability of wind turbines and their components and optimizing operation and maintenance (O&M) strategies. Increasing reliability and optimizing O&M have a direct impact on the availability of wind turbines and thus reduce cost and increase energy output. This stra ...
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 13

 TERMINÉ 

GReener Aeronautics International Networking-2 (GRAIN 2)

Date du début: 1 oct. 2013, Date de fin: 31 mai 2016,

As mentioned in the Executive Summary of the Strategic Research & Innovation Agenda, Aviation has an important role to play in reducing greenhouse gas emissions as well as noise and local air quality issues. The continuous increase of air passenger transport generates an increasing use of hydrocarbon fuel with excessive emission of CO2 and NOX (greenhouse gases, pollutants and noise). It is well k ...
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 25

 TERMINÉ 

Transition Location Effect on Shock Wave Boundary Layer Interaction (TFAST)

Date du début: 1 févr. 2012, Date de fin: 31 janv. 2016,

...de a characterization and selection of appropriate flow control methods for transition induction as well as physical models of these devices.Emphasis will be placed on closely coupled experiments and numerical investigations to overcome weaknesses in both approaches.
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 16

 TERMINÉ 

Development of multifunctional Thermal Barrier Coatings and modelling tools for high temperature power generation with improved efficiency (THEBARCODE)

Date du début: 1 janv. 2013, Date de fin: 31 déc. 2015,

This project is focused to advance considerably the efficiency of power generation in gas turbine processes by the development of improved thermal barrier coated parts or components of significantly improved performance as well as software products providing optimized process parameters.The proposed project addresses the following scientific and technological issues:New TBC formulations with long- ...
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 14

 TERMINÉ 

Advances in Numerical and Analytical tools for DEtached flow prediction (ANADE)

Date du début: 1 janv. 2012, Date de fin: 31 déc. 2015,

The present project is based on existing collaborations in different national and international projects, a common research interest toward fluid dynamics applied to industrial problems and existing, although immature, common training programs between the partners. We all partners agree that the current skills of science graduates in the technologies covered by this project are still insufficient ...
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 10

 TERMINÉ 

Numerical aero-acoustic assessment of installed Counter Rotating Open Rotor (CROR) power plant (NAA-CROR)

Date du début: 1 avr. 2011, Date de fin: 31 mai 2015,

"The inherently high propulsive efficiency of advanced propellers and Counter-Rotating Open Rotors (CROR) have a great potential for fuel savings, but the level of noise emitted by the open blades represent a major obstacle to their environmental acceptance. Consequently, the design of a low noise, fuel efficient open rotor powerplant is one of the major objectives in the CleanSky JTI. Within the ...
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 1

 TERMINÉ 

Engine Representative Internal Cooling Knowledge and Applications (ERICKA)

Date du début: 1 juil. 2009, Date de fin: 30 juin 2014,

"The goal of ERICKA is to directly contribute to reductions in aircraft engine fuel consumption with a targeted contribution of 1% reduction in SFC relative to engines currently in service. The fuel efficiency of a jet engine used for aircraft propulsion is dependent on the performance of many key engine components. One of the most important is the turbine whose efficiency has a large influence ...
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 20

 TERMINÉ 

Industrialisation of High-Order Methods – A Top-Down Approach (IDIHOM)

Date du début: 1 oct. 2010, Date de fin: 31 mars 2014,

"The proposed IDIHOM project is motivated by the increasing demand of the European aerospace industries to advance their CFD-aided design procedure and analysis by using accurate and fast numerical methods, so-called high-order methods. They will be assessed and improved in a top-down approach by utilising industrially relevant complex test cases, so-called application challenges in the general ar ...
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 21

 TERMINÉ 

Manipulation of Reynolds Stress for Separation Control and Drag Reduction (MARS)

Date du début: 1 oct. 2010, Date de fin: 31 mars 2014,

"Reynolds stress is the most important quantity affecting the mean flow as it is responsible for a major part of the momentum transfer in the wall bounded turbulent flow. It has a direct relevance to both skin friction and flow separation. Manipulation of the Reynolds stress can directly lead to changes in the viscous stress at the wall so as to effectively control the flow for effective flow cont ...
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 19

 TERMINÉ 

Efficient CFD Multi-physics programming research (E-CFD-GPU)

Date du début: 1 févr. 2011, Date de fin: 31 juil. 2013,

"The current evolution in the aeronautical field towards high-fidelity simulations, including multi-physics and more reliable modeling of turbulence and transition, calls for a new approach of the complete CFD-multi-physics simulation chain, with a drastic reduction of its turnaround time.This requires revising the whole CAE chain, from pre-processing (CAD handling and mesh generation), to very f ...
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 2

 TERMINÉ 

VALidation and Improvement of Airframe Noise prediction Tools (VALIANT)

Date du début: 1 sept. 2009, Date de fin: 31 mai 2013,

...reduction is essential for achieving the ACARE 2020 objectives of noise level reductions. However, the complexity and diversity of broadband turbulent noise sources makes that prediction with present numerical tools extremely challenging and far from mature. VALIANT is an upstream research-oriented project, with objective to tackle this challenge by generating new experimental data and validating ...
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 13

 TERMINÉ 

Future Fast Aeroelastic Simulation Technologies (FFAST)

Date du début: 1 janv. 2010, Date de fin: 31 mars 2013,

"The upstream FFAST project addresses the topic Design Systems and Tools (AAT.2008.4.1.1) by developing, implementing and assessing a range of numerical simulation technologies to accelerate future aircraft design. Critical load identification methods and reduced order modelling techniques developed will potentially provide a step change in the efficiency and accuracy of the dynamic aeroelastic “l ...
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 14

 TERMINÉ 

Combustion Models for Industrial Applications (COMBINA)

Date du début: 1 mars 2009, Date de fin: 28 févr. 2013,

... on longer term industrial objectives and provide additional test cases. The current COMBINA project opens new pathways across the different sectors. The coordinating SME-1 is having the most recent numerical combustion models integrated in its software system towards the demands of end users in the manufacturing industry. SME-2 will benefit from intensive exchanges and transfers on experimental ...
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 7

 TERMINÉ 

GReener Aeronautics International Networking (GRAIN)

Date du début: 1 oct. 2010, Date de fin: 31 déc. 2012,

"Aerochina1&2 have been networking projects co-funded by FP7 and AVIC (China) and coordinated by CIMNE. Many of the GRAIN partners have participated in them. These collaborative projects gathered experts on the two Europe (13) and China (17) sides to foster cooperation and debate future trends in the field of integrated multi physics modeling, computer simulations and code validation, experimental ...
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 18

 TERMINÉ 

Advanced Turbulence Simulation for Aerodynamic Application Challenges (ATAAC)

Date du début: 1 avr. 2009, Date de fin: 30 juin 2012,

"The ATAAC project aims at improvements to Computational Fluid Dynamics (CFD) methods for aerodynamic flows used in today’s aeronautical industry. The accuracy of these is limited by insufficient capabilities of the turbulence modelling / simulation approaches available, especially at the high Reynolds numbers typical of real-life flows. As LES will not be affordable for such flows in the next 4 d ...
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 22

 TERMINÉ 

Design of innovative CROR blade and pylon (DINNO-CROR)

Date du début: 1 janv. 2010, Date de fin: 31 janv. 2012,

...e capability of the CFD/CAA software systems. The present project combines an experimental investigation of two, low TRL flow/noise control options, associated with an innovative and highly efficient numerical CFD/CAA approach. On the experimental side, the first noise control method, based on porous treatment of the blades, will be tested in an anechoic facility. The associated acoustic impedance ...
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 2

 TERMINÉ 

Theories and Numerical code for prediction of near and far field noise generated by new generation propellers and Open Rotor blades (CAA-NLH)

Date du début: 1 janv. 2010, Date de fin: 30 sept. 2010,

"The inherently high propulsive efficiency of advanced propellers and Counter-Rotating Open Rotors (CROR) have a great potential for fuel savings, but the level of noise emitted by the open blades represent a major obstacle to their environmental acceptance. Consequently, the design of a low noise, fuel efficient open rotor powerplant is one of the major objectives of the CleanSky JTI. Within the ...
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 1

 TERMINÉ 

"Prospecting and promoting scientific cooperation between Europe and China in the field of multiphysics modeling, simulation, experimentation and design methods in aeronautics" (AEROCHINA2)

Date du début: 1 oct. 2007, Date de fin: 31 déc. 2009,

"The aim of the AEROCHINA2 Coordination Support Action (CSA) is to foster the cooperation between a number of industry, university and research organizations in the aeronautics sector in Europe and China in the field of multi-physics modelling, computer simulation and code validation, experimental testing and design methods for the solution of multi-physics problems of interest to the aeronautic s ...
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 14