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SUBLIME SIGNED

Supporting Understanding of Boundary Layer Ingesting Model Experiment

Total Cost €

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EC-Contrib. €

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Partnership

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 SUBLIME project word cloud

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

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Project "SUBLIME" data sheet

The following table provides information about the project.

Coordinator
UNIVERSITA DEGLI STUDI DI PADOVA 

Organization address
address: VIA 8 FEBBRAIO 2
city: PADOVA
postcode: 35122
website: www.unipd.it

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 Italy [IT]
 Total cost 3˙612˙549 €
 EC max contribution 3˙612˙549 € (100%)
 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 2019
 Duration (year-month-day) from 2019-12-01   to  2022-11-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI PADOVA IT (PADOVA) coordinator 25˙000.00
2    AIRCRAFT RESEARCH ASSOCIATION LIMITED UK (BEDFORD) participant 2˙559˙623.00
3    HIT09 SRL IT (PADOVA PD) participant 422˙562.00
4    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 394˙738.00
5    CHALMERS TEKNISKA HOEGSKOLA AB SE (GOETEBORG) participant 210˙625.00

Map

 Project objective

SUBLIME (Supporting Understanding of Boundary Layer Ingestion Model Experiment)

The introduction of engines integrated with the rear fuselage (BLI engines) in large passenger aircrafts poses new challenges regarding accurate experimental assessment of their performance, especially in terms of power savings, over conventional propulsive architectures (e.g. podded engines) as the engine is fed with a distorted flow. The SUBLIME project will address this challenge, resulting in a flexible and robust experimental set-up to establish dependencies among the propulsor shape/position, the fan inlet distortion pattern and the corresponding power savings. A consortium of an R&D institute, an SME, and 2 Universities with complementary skills will produce this result in close coordination with the topic manager in 36 months, asking for a grant of € 3.612.500. Coordinator ARA will provide a number of aircraft configurations equipped with BLI propulsors integrated in the rear fuselage, designed and optimized in cooperation with HIT09 (mainly responsible for CFD studies and fan design), Cranfield University (mainly responsible for theoretical and experimental force bookkeeping) and Chalmers University of Technology (mainly involved in engine cycle studies), to be subsequently manufactured and tested by ARA in their transonic wind tunnel. The project will advance the state of the art in BLI studies by means of wind tunnel activities supported by high-fidelity CFD simulations to consistently predict full-scale behaviour of the aircraft architectures suitable for appropriate propulsor installation which minimizes inlet flow distortions and maximizes power saving. The results of installed wind-tunnel tested aircraftpropulsors will be delivered in full compliance with the call. SUBLIME will provide methodologies, tools and facilities to the European aviation industry, therefore contributing to releasing the full potential of power saving of BLI engines.

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

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