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Acoustic Design Of High-lift Architectures

Objectif

Regulation of the sound production of aircraft is becoming stricter, in part due to an increase in the noise generated due to the rising numbers and size of aircraft. As a result identification and reduction of the major sources of sound, particularly in the take-off and landing phases when the aircraft is close to population centres, is paramount. High lift devices, particularly during the landing phase, are a major source of airframe noise. As a result there is a requirement for a tool to allow the acoustic properties of a high-lift configuration to be determined buring the design process. The purpose of this proposal is the development of such a tool.

Appel à propositions

SP1-JTI-CS-2009-01
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Coordinateur

AIRCRAFT RESEARCH ASSOCIATION LIMITED
Contribution de l’UE
€ 123 750,00
Adresse
MANTON LANE
MK41 7PF Bedford
Royaume-Uni

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Région
East of England Bedfordshire and Hertfordshire Bedford
Type d’activité
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Contact administratif
David Lawrie (Dr.)
Liens
Coût total
Aucune donnée

Participants (1)