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The BALANCE project focuses on improving the aerodynamic efficiency of business jet nacelles by extending laminar airflow. It aims to reduce drag by optimizing nacelle design and integration with engines, ultimately enhancing performance while controlling production and operating costs.
Development of nacelle concepts to allow increased laminar airflow over a business jet nacelle.
The technologies developed through this project will achieve 1% drag at aircraft level, through extension of the laminar surface to 30-40% of the nacelle length.BALANCE will investigate means of reducing the number of aerodynamic disturbances present in the forward portion of the nacelle, including reviewing interface locations, methods of attaching parts, and impacts on engine integration to ensure…
SAFRAN NACELLES
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