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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.

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

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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