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ASTORIA SIGNED

Advanced Steady and unsTeady distORtion sImulAtor

Total Cost €

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EC-Contrib. €

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Partnership

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 ASTORIA project word cloud

Explore the words cloud of the ASTORIA project. It provides you a very rough idea of what is the project "ASTORIA" about.

position    practices    extensive    distortion    combined    baseline    toolset    screens    designs    precisely    demonstrated    jti    swirl    01    intent    integrating    periodic    answering    engine    minimization    assemblies    vanes    fully    unprecedented    generating    boundary    lpa    screen    rig    applicable    steady    conversely    sa    layer    replicating    turning    jointly    limit    subset    iadp    astoria    optimization    cfp09    airframe    rapid    vane    environment    base    definition    dx2    capability    software    will    preserve    unsteady    fan    fir    variation    tools    cs2    flexible    paving    profiles    59    total    replication    manufacturability    simulation    validated    size    solutions    demonstrator    undesirable    assembly    models    fidelity    influence    modular    seamlessly    rotate    shapes    pressure    frame    limitless    tested    cfd    experimental    serve    patterns    mechanical    sup2    effect    linked    prototyping    pattern    aerodynamic    integrate    wp1    arbitrarily    fixed    ingestion    possibilities    2018    parts    device    combine    harnessing    generator    envisaged   

Project "ASTORIA" data sheet

The following table provides information about the project.

Coordinator
CENTRE DE RECHERCHE EN AERONAUTIQUE ASBL - CENAERO 

Organization address
address: Batiment Eole, 1er étage - rue des Frères Wright 29
city: GOSSELIES
postcode: 6041
website: www.cenaero.be

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 Belgium [BE]
 Total cost 2˙378˙125 €
 EC max contribution 2˙200˙000 € (93%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP09-2018-02
 Funding Scheme CS2-IA
 Starting year 2019
 Duration (year-month-day) from 2019-10-01   to  2023-08-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    CENTRE DE RECHERCHE EN AERONAUTIQUE ASBL - CENAERO BE (GOSSELIES) coordinator 700˙000.00
2    INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES BE (RHODE SAINT GENESE) participant 1˙100˙000.00
3    NUMERICAL MECHANICS APPLICATIONS INTERNATIONAL SA BE (BRUXELLES) participant 400˙000.00

Map

 Project objective

Fully answering the requirements of topic JTI-CS2-2018-CfP09-LPA-01-59, the ASTORIA project aims at developing a demonstrated set of tools and methodologies in order to design and test devices replicating complex, steady and unsteady, total pressure and swirl combined distortion profiles with high fidelity in a test rig environment. Software and methodologies will be developed that will enable the definition of tailored multi-component devices, based on extensive exploitation of CFD, reduced-order models and optimization, harnessing the potential offered by rapid prototyping. Steady and unsteady patterns design methodologies will be validated through extensive experimental reduced-scale testing in precisely controlled conditions. The software toolset will be highly modular and flexible. The objective is to combine into a new multi-component distortion generator generic total pressure distortion generating screens and aerodynamic turning vanes assemblies, with limitless possibilities in vane shapes, distribution and size for complex swirl pattern replication. Several assembly solutions are envisaged, which will allow to jointly rotate parts (swirl frame and base distortion) or, conversely, preserve a fixed baseline steady distortion pattern and limit periodic position variation to a subset of turning vanes and/or screen. The integrated toolset will provide an unprecedented capability for combined arbitrarily complex total pressure and swirl distortion simulation, including the minimization of the undesirable influence of the device and directly integrating mechanical and manufacturability into the design intent. It will also seamlessly allow to integrate the potential effect of the fan. ASTORIA is specifically linked with LPA-IADP-WP1.1.3.6, will directly be applicable for specific fan designs to be tested within the SA²FIR rig and will serve the “DX2 Boundary Layer Ingestion” demonstrator, paving the way for new robust integrated engine/airframe design practices.

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

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