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Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control
Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control
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机译:优化的机舱轮廓和气室形状,用于边界层摄入主动层流控制
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摘要
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.
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