Lift Recovery for AFC-Enabled High Lift System

Lift Recovery for AFC-Enabled High Lift System

This project is a continuation of the NASA AFC-Enabled Simplified High-Lift System Integration Study contract (NNL10AA05B) performed by Boeing under the Fixed Wing Project. This task is motivated by the simplified high-lift system, which is advantageous due to the simpler mechanical system, reduced...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Shmilovich, Arvin, Yadlin, Yoram, Dickey, Eric D., Gissen, Abraham N., Whalen, Edward A.
Format: Report
Sprache:eng
Schlagworte:
Aerodynamics
Fluid Mechanics And Thermodynamics
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Beschreibung
Zusammenfassung:This project is a continuation of the NASA AFC-Enabled Simplified High-Lift System Integration Study contract (NNL10AA05B) performed by Boeing under the Fixed Wing Project. This task is motivated by the simplified high-lift system, which is advantageous due to the simpler mechanical system, reduced actuation power and lower maintenance costs. Additionally, the removal of the flap track fairings associated with conventional high-lift systems renders a more efficient aerodynamic configuration. Potentially, these benefits translate to a approx. 2.25% net reduction in fuel burn for a twin-engine, long-range airplane.