ACRONYM: COJEN
Computation of Coaxial Jet Noise
Sitemap Rail Traffic
Sitemap Road Traffic
Sitemap Air Traffic
Sitemap Outdoor Equipment
Sitemap Maritime Traffic
Sitemap Health Aspects
Sitemap Noise Exposure
  General Information

The principle objective of COJEN is to develop and validate prediction tools that can be used by the aerospace industry to assess and optimise jet-noise reduction techniques. COJEN will deliver the enabling technology to allow European Aerospace industries to:

  • design lower-noise aircraft to meet society's needs for more environmentally friendly air transport
  • win global leadership for European aeronautics, with a competitive supply chain.

More specifically, COJEN will deliver the methods for designing concepts and technologies for the reduction of aero-engine jet noise, whilst improving industry's ability to competitively develop new products and reduce development time and cost. In order to bring the fundamental work of the FP5 project JEAN (which aimed at prediction of single-stream jet noise) and other programmes to the point where they are useful to industry, the methods developed therein must be extended to cope with hot coaxial jets and arbitrary nozzle geometries. The methods must also be validated to demonstrate their accuracy and reliability. Accordingly, the specific technical objectives of the project are to:

  • identify and improve optimal CFD techniques for the prediction of jet flow development from coaxial nozzles of arbitrary geometry
  • develop aero-acoustic codes which can predict the acoustic fields from the CFD results
  • acquire aerodynamic and acoustic data adequate to validate these codes.

To achieve these objectives, two approaches will be considered. The first is the classical indirect technique in which the turbulent flow field is characterised using a CFD solver and the acoustic modelling uses information extracted from the spatially-resolved turbulence field (local intensity and length scales of the turbulence) to predict the far field noise. The second is the direct computational approach in which Large Eddy Simulation (LES) methods will be used to determine the near field noise.

  Project Data
Project Type: EU Project
Project Ref. No.: 502790
Duration: 1 Feb. 2004 - 1 Feb. 2007
Main Contractor: QINETIQ LIMITED
Contact Person: Craig Mead
  Tel: +44-0125-2397738
Costs: 5,691,810 €
Project Homepage: www.x-noise.net/associatedprojects/generation2.htm
  Partners (24)
CENTRALE LYON INNOVATION - CLI  FR
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE  FR
CHALMERS TEKNISKA HÖGSKOLA  SE
DASSAULT AVIATION SA  FR
DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V. - DLR  DE
ECOLE CENTRALE DE LYON  FR
INDUSTRIA DE TURBO PROPULSORES S.A.  ES
INTEGRATED AEROSPACE SCIENCES CORPORATION O.E.  GR
LOUGHBOROUGH UNIVERSITY OF TECHNOLOGY  UK
NATIONAL RESEARCH & DEVELOPMENT INSTITUTE FOR TURBOENGINES COMOTI R.A.  RO
OFFICE NATIONAL D'ÉTUDES ET DE RECHERCHES AÉROSPATIALES - ONERA  FR
QINETIQ LIMITED  UK
RHEINISCH WESTFÄLISCHE TECHNISCHE HOCHSCHULE AACHEN  DE
ROLLS ROYCE DEUTSCHLAND LTD&CO KG  DE
ROLLS ROYCE PLC  UK
TECHNISCHE UNIVERSITÄT BERLIN  DE
TRINITY COLLEGE DUBLIN  IE
UNIVERSIDAD CARLOS III DE MADRID  ES
UNIVERSIDAD POLITECNICA DE MADRID  ES
UNIVERSITE DE POITIERS  FR
UNIVERSITY OF BATH  UK
UNIVERSITY OF SOUTHAMPTON  UK
UNIVERSITY OF WARWICK  UK
VOLVO AERO CORPORATION AB  SE
  Download
PDF File for Printout and/or Download

Left Click: "Open PDF ... "   •   Right Click: "Save Target as ... "