Model Design and Manufacturing of the Turbofan Configuration for Low Speed Aerodynamic and Acoustic Testing

Projektinformationen

LOSPA

ID Finanzhilfevereinbarung: 271815

Abgeschlossenes Projekt

Startdatum 1 November 2011

Enddatum 31 Dezember 2014

Finanziert unter

• Specific Programme "Cooperation": Joint Technology Initiatives

Gesamtkosten € 1 305 005,60

EU-Beitrag € 978 753,70

Koordiniert durch

AIRCRAFT RESEARCH ASSOCIATION LIMITED
United Kingdom

Ziel

"A requirement has been produced to design and manufacture an innovative new wind tunnel model to enable the acquisition of aerodynamic and acoustic data. Nacelles and pylons will be included to accommodate two turbofan simulators which are to be supplied by DNW/ONERA. A set of wings will be produced which will have removable leading edges and trailing edge flaps. This will allow a wide range of configurations to be investigated, including clean, take-off, landing and airbrakes on/off. A modular empennage will also be produced. These items will be designed to interface with the remainder of the model which will be provided by a partner independent of this CFP. The resultant model will be tested in a low speed wind tunnel at atmospheric pressure to investigate two topics. Firstly, the effectiveness of the empennage in shielding engine noise, and secondly the assessment of wing aerodynamic efficiency together with low speed take-off and landing performance and handling qualities. A large number of steady and unsteady probes will be installed in the model. Kulites ® will be mounted in the thin nacelle and empennage. These will be supplemented by gauges on the empennage to measure loads.

Aircraft Research Association (ARA) proposes to apply its extensive experience in wind tunnel model design and manufacture. ARA will lead the programme of work with manufacturing support provided by Future Advanced Manufacturing Ltd (FAM). ARA and FAM have worked closely on many wind tunnel model programmes, producing high quality models to exacting tolerances and demanding timescales. Over many years, ARA and FAM have established reliable working practices, innovative technical solutions to challenging requirements and effective project control and management processes. ARA and FAM will apply this expertise to the requirements of this new call to ensure that all aspects of the model are achieved in the required timescale and budget.
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Wissenschaftliches Gebiet

• engineering and technology › mechanical engineering › vehicle engineering › aerospace engineering › aircraft
• natural sciences › physical sciences › acoustics
• natural sciences › earth and related environmental sciences › atmospheric sciences › meteorology › atmospheric pressure

Programm/Programme

• FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives

Thema/Themen

• JTI-CS-2010-3-SFWA-02-009 - Model design & manufacturing of the turbofan configuration for low speed aerodynamic and acoustic tests

Aufforderung zur Vorschlagseinreichung

SP1-JTI-CS-2010-03
Andere Projekte für diesen Aufruf anzeigen

Finanzierungsplan

JTI-CS - Joint Technology Initiatives - Clean Sky

Koordinator

AIRCRAFT RESEARCH ASSOCIATION LIMITED

Kontakt Verwaltung

Paul Hammond (Mr.)

• EU-Beitrag: € 688 753,00
• Adresse: MANTON LANE ; MK41 7PF Bedford ; Vereinigtes Königreich
• Region: East of England › Bedfordshire and Hertfordshire › Bedford
• Aktivitätstyp: Private for-profit entities (excluding Higher or Secondary Education Establishments)
• Gesamtkosten: Keine Daten

Beteiligte (1)

FUTURE ADVANCED MANUFACTURE LTD

Vereinigtes Königreich

Kontakt Verwaltung

Mike Sullivan (Mr.)

• EU-Beitrag: € 290 000,70
• Adresse: BAMFURLONG INDUSTRIAL PARK 16-18 ; GL51 6SX CHELTENHAM
• Aktivitätstyp: Private for-profit entities (excluding Higher or Secondary Education Establishments)
• Gesamtkosten: Keine Daten