In one embodiment, an airfoil includes a first end and a second end opposite the first end. The airfoil also includes a first side and a second side opposite the first side. The airfoil includes a continuous panel coupled to the first side of the airfoil. The continuous panel includes a first edge having a first uneven edge pattern. The first edge has at least four vertices disposed thereon. The continuous panel extends from the first end of the airfoil to a second end of the airfoil.
Panels comprising uneven edge patterns for reducing boundary layer separation
2019-09-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
PANELS COMPRISING UNEVEN EDGE PATTERNS FOR REDUCING BOUNDARY LAYER SEPARATION
Europäisches Patentamt | 2019
|Panels Comprising Uneven Edge Patterns for Reducing Boundary Layer Separation
Europäisches Patentamt | 2017
|Patterns of three-dimensional boundary layer separation
AIAA | 1987
|PANEL HAVING NON-UNIFORM EDGE FOR REDUCING BOUNDARY LAYER PEELING
Europäisches Patentamt | 2017
|