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
29.01.2019
Patent
Elektronische Ressource
Englisch
OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL
Europäisches Patentamt | 2016
|OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL
Europäisches Patentamt | 2019
|OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL
Europäisches Patentamt | 2021
|