The present disclosure is directed to a rotatable fairing panel at a rear end of a sleeper cab. The rotatable fairing panel covers an opening between a trailer attached to a vehicle and the sleeper cab of the vehicle. The rotatable fairing panel has a closed position and an opened position. At least one locking assembly locks the rotatable fairing panel in place when in the closed position. The at least one locking assembly is configured to be unlocked by a user such that the rotatable fairing panel may be rotated from the closed position to the opened position such that a user may access the opening between the trailer attached to the vehicle and the sleeper cab of the vehicle. The at least one locking assembly automatically locks when the user rotates the rotatable fairing panel into the closed position.

Disclosed are systems and techniques for increasing heat transfer from a substrate to a working fluid. The systems may include a substrate comprising a plurality of grooves or cavities on at least one external surface. The system may also include an infusing liquid filling at least a majority of the plurality of grooves. The system may also include a working fluid configured to flow parallel to the external surface.

This relates to the field of aerohydrodynamics and can be used on wings and control surfaces of aircraft, controlled spoilers of sports cars, all-movable masts and sails of sailing yachts and sailboards, as well as on blades and vanes of various bladed machines. An aerohydrodynamic surface includes an array of vortex generators and a main part. The main part comprises two sides mating with each other to form a leading and a trailing edges. The array of vortex generators includes elevations with crescent-shaped working edges located near the leading edge. The elevations and the working edges are configured to generate counter-rotating vortex structures. An array of vortex generators and a method of mounting the same onto the aerohydrodynamic surface are also described. The invention makes it possible to improve the properties of the aerohydrodynamic surfaces at high angles of attack.

Microstructured surface development three dimensional form solutions that provide multiple functional benefits when applied to an object. Microstructured surface development three dimensional form solutions that provide efficiency gains to an object in dynamic motion in a fluid medium through aerodynamic/hydrodynamic skin friction drag reduction. Microstructured surface development three dimensional form solutions that additionally provide functional benefits to an object in a static, non-moving state as well as a dynamic state—namely super-hydrophobicity, light absorption, sound/radar absorption and heat dissipation. Microstructured surface development three dimensional form solutions that can be molded into the surface of an object. Microstructured surface development three dimensional form solutions that can be added to the surface of an object though a secondary forming operation (ie machining, laser engraving). Microstructured surface development three dimensional form solutions that can be attached to the surface of an object using an adhesive backed thin film that has been molded/cast with unique microstructured surfaces. Microstructured surface development three dimensional form solutions that are composed of unique tile-like individual elements that can be assembled as a unique continuous array on an object.

A magnetic insertion meter is disclosed herein. Disclosed insertion meters include in some examples, a sensor head tube cylinder having a textured front surface and at least two electrodes. Disclosed insertion meters include a textured front surface adapted to move the separation point of a fluid flowing over the sensor head tube towards the upstream surface as compared to the same sensor head tube without the textured front surface. Methods of measuring flow are also disclosed herein using example magnetic insertion meters.

Microstructured surface development three dimensional form solutions that provide multiple functional benefits when applied to an object. Microstructured surface development three dimensional form solutions that provide efficiency gains to an object in dynamic motion in a fluid medium through aerodynamic/hydrodynamic skin friction drag reduction. Microstructured surface development three dimensional form solutions that additionally provide functional benefits to an object in a static, non-moving state as well as a dynamic state—namely super-hydrophobicity, light absorption, sound/radar absorption and heat dissipation. Microstructured surface development three dimensional form solutions that can be molded into the surface of an object. Microstructured surface development three dimensional form solutions that can be added to the surface of an object though a secondary forming operation (ie machining, laser engraving). Microstructured surface development three dimensional form solutions that can be attached to the surface of an object using an adhesive backed thin film that has been molded/cast with unique microstructured surfaces. Microstructured surface development three dimensional form solutions that are composed of unique tile-like individual elements that can be assembled as a unique continuous array on an object.

The present disclosure relates to a device and a method for swinging power generation and vibration suppression by using arc-shaped wing plates with rough surfaces. The device consists of two parts, namely, a rotary swinging system and a collector system. The rotary swinging system includes a collector riser, steering bearings, nanometer material arc-shaped power generation wing plates, and flexible tail plates. The collector system includes telescopic power generation cylinders, a waterproof electric slip ring, and a waterproof power transmission line. The suppression of energy-consumption-free vortex-induced vibration is realized under the combined action that the nanometer material arc-shaped power generation wing plates divide a flowing space and adjust a flow direction, the nanometer material arc-shaped power generation wing plates drive the flexible tail plates to swing to destroy a tail vortex street, and hemispherical bulges and trumpet-shaped deflector holes disturb a boundary layer around flow.

A device for lacquer transfer includes a frame, a transfer roller with a circumferential lateral wall, a drive unit and a lacquer application unit. The lacquer application unit is mounted on the frame and applies lacquer to a work surface of a work piece while the device is moved in an application direction across the work surface. The drive unit drives the transfer roller in a rotation direction about an axis of rotation. An outside contact surface of the lateral wall comprises a plurality of depressions forming a predetermined structure. The transfer roller rolls with the outside contact surface on the work surface of the work piece for transferring the predetermined structure defined by the depressions in the outside contact surface to lacquer previously applied to the work surface by the lacquer application unit.

A flow modification device connectable to a generally cylindrical element adapted for immersion in a fluid medium is provided. The device comprises an elongate body having a length and a generally circular cross-section; a plurality of raised body portions disposed about and extending along the length of the elongate body, the raised body portions having a height between 2% and 10% of a diameter of the body; and an aperture extending through the length of the elongate body, the aperture being adapted to receive the generally cylindrical element such that the flow modification device is arranged about the cylindrical element. The plurality of raised body portions are helically arranged or twisted about a longitudinal axis of the elongate body and are adapted to reduce vortex-induced vibration and/or drag on the cylindrical element when the device is connected to the cylindrical element and the connected device and cylindrical element are immersed in the fluid medium and there is relative movement between the connected device and cylindrical element and the fluid medium.

Provided are: an adhesive sheet-shaped member for airflow, in an optimum form that can improve fuel efficiency and travel performance as a result of more effectively suppressing a large airflow separation phenomenon that becomes air resistance; and a travel vehicle using the same. A sheet-shaped member that is: provided thinly so as to prevent, as far as possible, the thickness thereof providing air resistance; adhered to a surface in contact with an airflow provided by a material that charges negative static electricity; formed in a long sheet shape in a flow direction of airflow, compared to the width direction of the airflow, so as to be adhered along the direction of the airflow; and provided using a material that charges a negative static electricity and has a different ease of static electrical charge than the surface in contact with the airflow.