Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing

This application is based on and claims the priority under 35 U.S.C. §119 of German Patent Application 101 57 849.0, filed on Nov. 24, 2001, the entire disclosure of which is incorporated herein by reference. A slat is selectively extended from a main wing body, with a concave rear surface of the sl...

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Hauptverfasser:	Mau, Knut, Dobrzynski, Werner
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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