Aerodynamic and acoustic capabilities developments for close coupling, high bypass ratio turbofan Aircraft integration

In order to prepare the capabilities for future Powerplant system integration into Aircraft, the applicant will extend existing numerical capabilities to be able to tackle the specificities of those integrations: strong coupling between Powerplant and Aircraft; Reduced size nacelles; Low drag nacelle solutions.  Please refer for the full and formal topic description to Annex III of the Clean Sky 2 Work Plan 2014-2015 Amendment nr. 1  Version 3 (see under the tab ""Topic Conditions and Documents"")