Opendata, web and dolomites

NIFTI SIGNED

Non-Intrusive Flow distortion measurements within a Turbofan Intake

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 NIFTI project word cloud

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

tolerant    least    spatial    aircraft    industrial    engine    automated    representative    structural    short    operation    notable    closely    rules    upstream    nifti    coupled    off    adversely    integrity    designs    measuring    numerical    bubbles    technique    certification    potentially    unlock    3d    filled    entire    aerodynamics    resolution    baseline    unsteady    fan    gap    reduce    soap    bypass    slim    ratio    angle    magnitude    ultimately    flexible    outputs    aero    engines    rely    plane    synchronous    intrusive    margin    wind    limitations    configurations    risk    ptv    practices    operability    camera    diameter    solution    flow    hfsb    distortion    inadequate    velocity    levels    attack    measured    located    stall    never    campaigns    helium    experimental    environment    distortions    performance    data    characterise    catastrophic    nature    datasets    propulsion    cross    demonstrating    pressure    intake    safety    technologies    aid    outcomes   

Project "NIFTI" data sheet

The following table provides information about the project.

Coordinator
STICHTING DUITS-NEDERLANDSE WINDTUNNELS 

Organization address
address: VOORSTERWEG 31
city: Marknesse
postcode: 8316 PR
website: www.dnw.aero

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 Netherlands [NL]
 Total cost 2˙336˙394 €
 EC max contribution 2˙250˙000 € (96%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP09-2018-02
 Funding Scheme CS2-RIA
 Starting year 2020
 Duration (year-month-day) from 2020-01-01   to  2022-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    STICHTING DUITS-NEDERLANDSE WINDTUNNELS NL (Marknesse) coordinator 1˙414˙324.00
2    LAVISION GMBH DE (GOETTINGEN) participant 538˙568.00
3    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 177˙355.00
4    IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE UK (LONDON) participant 119˙753.00

Map

 Project objective

Short and slim aero-engine intake designs for very high bypass ratio configurations cause notable levels of unsteady distortions at the fan face especially under cross-wind or angle of attack operation during aircraft take-off. Such distortions can adversely affect the engine’s performance, operability, structural integrity and safety margin with potentially catastrophic consequences for the entire propulsion system. Current practices for aero-engine testing and certification rely on a low number of intrusive pressure measurements at the fan face to characterise the distortion levels. Given the known limitations of currently used methods (low spatial resolution, intrusive nature) the existing technologies are inadequate to reduce the risk on the development and certification of future novel systems. NIFTI aims to address this gap by demonstrating a non-intrusive technique to measure velocity fields across a plane located upstream of a large diameter fan of a high bypass ratio aero-engine which has never been achieved. This method will provide synchronous datasets across the measurement plane with at least one order of magnitude higher spatial resolution than current methods. The implementation will demonstrate a highly automated and flexible multi-camera system within a representative industrial test environment. A number of more advanced, non-intrusive measuring technologies will be assessed such as 3D PTV or Helium Filled Soap Bubbles (HFSB) to further enhance the outputs of the selected baseline solution. The experimental activities will be supported by numerical campaigns and advanced data processing and flow analysis methods that will be used to analyse the highly unsteady nature of the flow distortions that will be measured during NIFTI’s experimental campaigns. These outcomes will ultimately unlock the complex aerodynamics of closely coupled fan-intake systems and aid the development of novel design rules for future, stall-tolerant aero-engines.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "NIFTI" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

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

More projects from the same programme (H2020-EU.3.4.5.1.)

CERES (2020)

advanCEd REar end Structural test program – low level tests

Read More  

ANACO (2018)

Advance Nacelle Aerodynamic Optimisation

Read More  

PROTEUSS (2019)

Pressurised Rotational Oil Transfer – Experimental Unit & System

Read More