Aspects of the disclosure are directed to a nacelle of an aircraft, comprising a surface that is profiled such that during cruise flight operation lines of constant static pressure of a boundary layer around the nacelle in a given region are substantially contained within a plane that is normal to an engine axis.
Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control
2019-01-29
Patent
Elektronische Ressource
Englisch
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