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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.

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

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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