Abstract
This article describes the design and optimization of a high-lift system for a forward swept wing intended for an environmentally friendly short-range aircraft concept studied in the EU project New Aircraft Concept REsearch, NACRE. The work presented here was carried out by FOI and aims at conceptual design an innovative high-lift system for a Natural Laminar Airfoil. The proposed designed high-lift system uses a droop nose on leading edge and a single Fowler flap on trailing edge. The performance of the high-lift system was further enhanced by a flow control.
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