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U-HARWARD SIGNED

Ultra High Aspect Ratio Wing Advanced Research and Designs

Total Cost €

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EC-Contrib. €

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Partnership

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Project "U-HARWARD" data sheet

The following table provides information about the project.

Coordinator
POLITECNICO DI MILANO 

Organization address
address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133
website: www.polimi.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 2˙510˙938 €
 EC max contribution 2˙510˙938 € (100%)
 Programme 1. H2020-EU.3.4.5.10. (Thematic Topics)
 Code Call H2020-CS2-CFP10-2019-01
 Funding Scheme CS2-RIA
 Starting year 2020
 Duration (year-month-day) from 2020-05-01   to  2023-10-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    POLITECNICO DI MILANO IT (MILANO) coordinator 581˙250.00
2    IBK-INNOVATION GMBH & CO. KG DE (HAMBURG) participant 561˙250.00
3    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES FR (PALAISEAU) participant 540˙192.00
4    UNIVERSITY OF BRISTOL UK (BRISTOL) participant 372˙746.00
5    SIEMENS INDUSTRY SOFTWARE SAS FR (CHATILLON) participant 322˙500.00
6    INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE FR (TOULOUSE) participant 133˙000.00

Map

 Project objective

U-HARWARD will consider the use of innovative aerodynamic and aeroelastic designs in a multi-fidelity multi-disciplinary optimal design approach to facilitate the development of Ultra-High aspect ratio wings for large transport aircraft. A conceptual design study, building on the current state of the art, will perform trade-off studies to determine the potential gains of different wing configurations and loads alleviation concepts in terms of aerodynamics, weight, noise, fuel-burn and range. Scaled model wind tunnel tests will be used to validate parametric variations in the aerodynamic and acoustic characteristics. Starting from a reference aircraft, the preliminary design of the best candidate configuration will be completed and the estimated gains validated using high fidelity tools and a larger scale aeroelastic test.

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The information about "U-HARWARD" are provided by the European Opendata Portal: CORDIS opendata.

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