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Model of surface, transverse or longitudinal surface increase of surfaces responsible for generating thrust, lift, propulsion or drag, such as airplane wings, airfoils and propeller blades
Model of surface, transverse or longitudinal surface increase of surfaces responsible for generating thrust, lift, propulsion or drag, such as airplane wings, airfoils and propeller blades
Model of increased surface area, transverse or longitudinal, of surfaces responsible for generating thrust, lift, propulsion or drag, such as aircraft wings, airfoils and propeller blades. The present invention relates to a model of increasing the transverse or generally longitudinal surface area of mechanisms responsible for generating thrust, lift, propulsion or drag. The surface with increased area by surface evagination and surface invagination of metals, polymers or other matrices is attached to the wings of airplanes, airfoils or other mechanisms, which provides substantial increase in surface area and boundary layer.
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