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Design, Simulation and Flight Reynolds Number Testing for Advanced High-Lift Solutions

Design, Simulation and Flight Reynolds Number Testing for Advanced High-Lift Solutions

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DeSiReH focus on both, the numerical design tools and the experimental measurement techniques for cryogenic conditions, with the objective to improve the industrial design process for laminar wings in terms of product quality, efficiency, and development cost reduction. The work focuses on the design of high lift devices. DeSiReH addresses the following quantified objectives which will make a significant contribution to meeting Vision 2020 goals: 1) Reduction of industrial A/C development costs by 5% by reduced and more efficient Wind Tunnel Testing 2) Decrease time-to-market by 5% by improved aerodynamic design turn-around time 3) Improve industrial High-Lift design process efficiency by 15% 4) Reduce A/C drag by 5% by enabling NLF though compatible High-Lift-Design To accomplish these objectives the project is planned for a period of 4 years and a budget of 7.6 Mio. Euro. The consortium consists of 6 industry partner, 7 research establishments, 3 universities, 2 small and medium-sized enterprise and the European Transonic Wind tunnel (ETW). Existing and validated high-fidelity numerical tools are composed to an efficient High-Lift design and optimization process chain in WP1. The strategies and tools developed are applied in WP 2 to the aerodynamic design of a high lift system for the future pointing HARLS wing (High Aspect Ratio Low Sweep) with the constraint to maintain Natural Lamiar Flow at cruise to the best possible extend. WP 3 focuses on the improvement of the experimental measurement technique for cryogenic testing. The objectives here are to enhance the measurement accuracy of the results and to generate the capability to apply different important techniques (e.g. transition measurement & deformation measurement). These techniques are finally applied in the ETW at High-Reynolds-Numbers on the HARLS model equipped with the High-Lift-System, designed in WP2. The final assessment of DeSiReH results is done in WP4 by assessing the numerical
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Koordinator

DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV

Adresse

Linder Hoehe
51147 Koeln

Deutschland

Aktivitätstyp

Research Organisations

EU-Beitrag

€ 958 663

Kontakt Verwaltung

Petra Rodenwaldt (Ms.)

Beteiligte (20)

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AIRBUS OPERATIONS GMBH

Deutschland

EU-Beitrag

€ 274 625

AIRBUS DEFENCE AND SPACE SA

Spanien

EU-Beitrag

€ 99 500

DASSAULT AVIATION

Frankreich

EU-Beitrag

€ 134 000

PIAGGIO AERO INDUSTRIES SPA

Italien

EU-Beitrag

€ 93 512

ASCO INDUSTRIES N.V.

Belgien

EU-Beitrag

€ 59 409

AIRCRAFT DEVELOPMENT AND SYSTEMS ENGINEERING (ADSE) BV

Niederlande

EU-Beitrag

€ 39 750

EUROPEAN TRANSONIC WINDTUNNEL GMBH

Deutschland

EU-Beitrag

€ 760 715

IBK-INNOVATION GMBH & CO. KG

Deutschland

EU-Beitrag

€ 288 400

CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA

Italien

EU-Beitrag

€ 365 944

TOTALFORSVARETS FORSKNINGSINSTITUT

Schweden

EU-Beitrag

€ 476 625

STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM

Niederlande

EU-Beitrag

€ 245 250

INSTITUTO NACIONAL DE TECNICA AEROESPACIAL ESTEBAN TERRADAS

Spanien

EU-Beitrag

€ 85 759

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

Frankreich

EU-Beitrag

€ 497 008

FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY

Russland

EU-Beitrag

€ 116 250

TECHNISCHE UNIVERSITAET BRAUNSCHWEIG

Deutschland

EU-Beitrag

€ 157 477

UNIVERSITA DEGLI STUDI DI NAPOLI FEDERICO II

Italien

EU-Beitrag

€ 83 112

UNIVERSITA DEGLI STUDI DI PADOVA

Italien

EU-Beitrag

€ 50 250

DR. DZIOMBA BERNHARD - DZIOMBA AERONAUTICAL CONSULTING

Deutschland

EU-Beitrag

€ 80 000

AIRBUS OPERATIONS SAS

Frankreich

EU-Beitrag

€ 126 086

IBK INGENIEURBUERO HAUPTSITZ

Deutschland

Projektinformationen

ID Finanzhilfevereinbarung: 233607

Status

Abgeschlossenes Projekt

  • Startdatum

    1 März 2009

  • Enddatum

    30 Juni 2013

Finanziert unter:

FP7-TRANSPORT

  • Gesamtbudget:

    € 7 078 825

  • EU-Beitrag

    € 4 992 335

Koordiniert durch:

DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV

Deutschland