CASCADE VANE LEADING EDGE

Aspects of the disclosure are directed to a cascade vane for an aircraft, comprising: a leading edge that is configured to interface to a fluid flow, where the leading edge is associated with a first thickness that is proximate to the fluid flow, and where the leading edge is associated with a secon...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Pritekel Joshua, Whitaker Anthony, Wen Matthew
Format: Patent
Sprache:eng
Schlagworte:
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