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a drag-reducing rib

A technology of ribs and crests, which is applied in the field of improved rib drag reduction devices, can solve the problems of easy damage, difficulty in processing, and restrictions on the practical application of rib drag reduction technology, and achieve enhanced drag reduction effect and high drag reduction performance

Active Publication Date: 2016-02-10
INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The drag reduction effect of the traditional triangular cross-section rib is limited and is easily affected by the fillet of the peak and ridge. Although the blade-shaped rib has a better drag reduction effect and is not affected by the fillet of the rib tip, the rib with such a thin thickness (t=0.02s) Difficult to process, poor structural strength, easy to break in practical application
The above-mentioned rib structure in the prior art severely limits the practical application of rib drag reduction technology

Method used

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Embodiment Construction

[0026] The present invention will be further described in detail below in conjunction with the examples, the following examples are explanations of the present invention and the present invention is not limited to the following examples.

[0027] Such as Figure 2 to Figure 5 As shown, the drag-reducing rib structure of the present invention includes a base 1, a rib crest 2 and a rib trough 3, which are arranged on the surface of the flow object along the flow direction, and the space between two adjacent rib crests 1 forms a rib trough 2, Each of the rib crests 1 includes two side walls 11 and a top protrusion 12, the top protrusion 12 is a columnar protrusion extending upward along the apex edge line of the two side walls 11 perpendicular to the base plane 1, the The top of the columnar protrusion is a plane, the angle between the two side walls 11 and the base plane 1 is basically the same, and the cross section of the columnar protrusion is substantially rectangular; The ...

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Abstract

The invention provides a novel resistance reducing rib. According to the resistance reducing rib, a cutting edge rib is additionally arranged at the position of a sharp corner of the peak of a traditional rib, the advantages, of the cutting edge rib, of being high in resistance reduction performance and free of the influence of a machining round corner are combined, the machining difficulty is considered, and the structural strength is improved. By reasonably selecting the size parameters, such as the height of the rib, the included angle, the thickness of the cutting edge and the height of the cutting edge, of the cross section of the rub, influencing the flowing structure of a boundary layer, increasing the thickness of a viscous bottom layer and limiting the extension movement of streamwise vortices, the purpose of resistance reduction is achieved, the friction resistance on the surfaces of aircrafts, underwater vehicles and ground transportation vehicles is reduced, and the application prospect is broad.

Description

technical field [0001] The invention relates to an improved rib drag reduction device, which can be applied to aviation, spaceflight, navigation, ground transportation and pipeline internal flow, etc. field. Background technique [0002] The rib technology is derived from the rib structure of shark shield scales. This bionic structure has been proved by a large number of research works to have strong practicability and good drag reduction effect. In the prior art, it is believed that the ribs with drag reduction effect must have sharp peaks and ridges, and there is a certain relationship between the spacing and the low-speed strip spacing, that is, when h + ≤25 and s + ≤30( See figure 1 , h is the rib height, s is the rib spacing, υ is the kinematic viscosity, u τ is the friction velocity, τ w is the wall shear stress, ρ is the density of the fluid medium, and the superscript "+" indicates a dimensionless parameter in the wall unit, the same below), and s + = h + =1...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F15D1/12F15D1/06
Inventor 张明明刘志丰徐建中王国付
Owner INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI