Design and demonstration of a laminar nacelle concept for business jet

This topic is devoted to design and validate a structural concept of laminar nacelle. Target benefit is to increase the laminarity area up to 30%-40% of nacelle length by taking into account many constraints and functions and to achieve a gain of at least 1% drag at aircraft level compared to a classical design at same weight and effort in production and operation.  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"")