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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.

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

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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