GB2502514A - A drag reduction method and material - Google Patents
A drag reduction method and material Download PDFInfo
- Publication number
- GB2502514A GB2502514A GB1208081.8A GB201208081A GB2502514A GB 2502514 A GB2502514 A GB 2502514A GB 201208081 A GB201208081 A GB 201208081A GB 2502514 A GB2502514 A GB 2502514A
- Authority
- GB
- United Kingdom
- Prior art keywords
- holes
- windproof
- layer
- rows
- coating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0025—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply
- F15D1/0055—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising apertures in the surface, through which fluid is withdrawn from or injected into the flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0025—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply
- F15D1/003—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising surface features, e.g. indentations or protrusions
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D13/00—Professional, industrial or sporting protective garments, e.g. surgeons' gowns or garments protecting against blows or punches
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0025—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply
- F15D1/006—Influencing flow of fluids by influencing the boundary layer using passive means, i.e. without external energy supply comprising moving surfaces, wherein the surface, or at least a portion thereof is moved or deformed by the fluid flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/10—Influencing flow of fluids around bodies of solid material
- F15D1/12—Influencing flow of fluids around bodies of solid material by influencing the boundary layer
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D2400/00—Functions or special features of garments
- A41D2400/24—Reducing drag or turbulence in air or water
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D2500/00—Materials for garments
- A41D2500/20—Woven
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D2600/00—Uses of garments specially adapted for specific purposes
- A41D2600/10—Uses of garments specially adapted for specific purposes for sport activities
- A41D2600/104—Cycling
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D31/00—Materials specially adapted for outerwear
- A41D31/04—Materials specially adapted for outerwear characterised by special function or use
- A41D31/10—Impermeable to liquids, e.g. waterproof; Liquid-repellent
- A41D31/102—Waterproof and breathable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B15/00—Superstructures, deckhouses, wheelhouses or the like; Arrangements or adaptations of masts or spars, e.g. bowsprits
- B63B2015/0016—Masts characterized by mast configuration or construction
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Textile Engineering (AREA)
- Laminated Bodies (AREA)
- Manufacturing Of Multi-Layer Textile Fabrics (AREA)
Abstract
A method of reducing drag on a body 1 in an air stream 7 and a material 2 is provided. The method comprises the covering of the body 1 with a material 2 comprising , for example, a fleece spacer layer 3 covered in a woven layer of nylon which has a windproof coating 5 thereon. The material is breathable, allowing the formation of one or more elongate bubbles 8 beneath the surface of the windproof coating 5, the elongate bubbles 8 being aligned normally to the direction 6 of the air flow 7. A material for covering a body 1 comprising a spacer layer 3, a woven layer and a windproof coating 5 applied to the woven layer is also disclosed.
Description
Drag Reduction Method and Material This invention relates to a new drag reduction method and materials therefor. The method and materials are applicable to sports clothing where drag on body elements can be a significant factor in performance, or br providing a surface layer on a blunt body to reduce the wind drag on the body. Examples of applications of the material include cyclists' clothing and coverings for yacht masts to reduce wind drag.
According to the present invention a method of reducing drag on a body in and air stream comprises the step of covering the object with a material having a windproof coating thereon and forming one or more elongate bubbles beneath the surface of the windproof coating said elongate bubbles being aligned normally to the direction of the air flow.
In one embodiment the alignment of elongate bubbles subtends an angle of 713° to 95° to the direction of the air flow.
Preferably the material comprises a wind poof coating on a woven material itself over a spacer material.
The spacer material is normally between 2 and 4mm inclusive thick. The nature spacer material is not critical, although a fleece material would usually be deployed.
The woven material is conveniently nylon and the windproof coating conveniently polyurethane.
In this specification the word body means both a human body, a mammal or animal body, or an inanimate object.
In another embodiment the invention, a material to cover a body or an object or part of such a body or object comprises a wind poof coating on a woven material itself over a spacer material.
In one arrangement said a windproof layer has a plurality of rows of holes through which wind may enter and leave between the windproof layer and the body.
It has been found that in a method according to the invention, the material, will form a bubble on the surface of the body at an angle of about 7Q° to 95°to the wind direction causing the flow of wind around the body to break away from the surface of the body producing a streamline-like effect and reducing thedrag c*i the body.
Without the streamline effect the laminar flow of wind around the body would to continue around the body from an upstream surface to a downstream surface eventually to break away from the surface in a turbulent flow which is the source of significant drag.
When the windproof layer has holes, it has been found that holes of between about 1mm and 2 mm work effectively. Normally the holes are distributed in parallel rows in the material so that when the material is formed into an item of clothing or as a drag reduction layer for a blunt body the parallel rows are parallel to axis of a limb or other body part of the person, or, when used to reduce the drag of a blunt body, to the axis of the blunt body. It has been found that smaller sized holes shows the greatest reduction in the drag coefficient but the reduction occurs at a higher wind velocities than for a larger holes. Clearly there is the possibility ot tuning the material to the particular application envisaged Any combination of compatible windproof layer coating on a woven layer can be used. For clothing for cycle racing, a fleece covered with a more breathable material such as Lycra® coated with a windproof and waterproof layer, such as BemisTM, works well. The holes are made by laser, about 1.5mm in diameter arranged in rows; the holes on the rows are about 5mm apart. The rows themselves are about 5mm apart.
To explain the invention more fully, reference is made, by way of example only, to the accompanying drawings in which; Figure 1 shows a section showing the invention in operation; Figure 2 shows in side section a material having laser cut holes according to the invention; Figure 3 shows a top section of a material shown in figure 2; Figure 4 shows test rults obtained using a test piece comprising a rod of dodecagon cross section, covered with a material according to the invention and subject to a head on wind of increasing velocity In figure 1 a body, which in this case is a thick rod 1, illustrative of an arm or a yacht mast, is shown in cross section. The rod 1 is covered with a triple layer material 2, comprising a fleece spacer layer 3, covered with a woven layer nylon, which has been coated with polyurethane 5. The rod 1 with the material covering 2 is placed in an air flow 7 coming from a direction 6 towards the rod 1. As the speed of the air flow increases a pair of elongate bubbles 8 form in material 2. The alignment of the bubbles is normal to the air flow. The bubbles 8 cause the flow around the rod to become detached and stream away being the rod. This detached flow leads to a significant reduction in drag caused by the rod (as illustrated in figure 4 below). The angle 9 subtended by a line through the centre of the bubbles 8 to the centre of the rod to a line 10 through the centre of the rod normal to the direction 6 from which the air flow comes is initially between 20° and 10°,i(e. 70° to 80° to the direction 6 from which the air flow comes). As the speed of the air flow increases, the angle 9 decreases eventually to about -5° to the normal 10 4.e. about 95° to the direction from which the air flow is coming), at this point no further change occurs.
In figures 2 and 3, a material 11 to be used in the manufacture of the arms of a cyclist's racing suit is showrt It comprises a first layer of a breathable nylon material 13 (such as Lycra ®) coated with a windproof layer 15 which is also water and oil repellent. The nylon layer covers a fleece layer 14, 2mm to 4mm thick, next to the cyclist's skin. The layer 15 has been laser treated to form rows of small holes, each hole being about 1.5mm in diameter and separate from the adjacent holes in its row by about 5mm. The rows themselves are arranged around the arm or thigh of a cyclist, and separated by about 5 mm. In practice it is easier to manufacture the material with holes around the body parts of interest, even though only those holes up-wind of the body part will be effective. As a cyclist wearing the suit having the material of the invention in his its arms, thighs and/or legs, wind will pass the cyclist from the head on direction and will enter into the suitthrough holes in the forward rows of holes under the wind proof layer 15 and travel around the arm of the cyclist before leaving though rows at about +/-75° to thedirection of travel. This causes the material to lift very slightly from the arm of the cyclist, effectively forming a deflector in a line parallel to the axis of the arm of the cyclist so diverting the air flow away from the rear of his/her arm, and reducing drag thereon.
Figure 3 shows the results of trails using a rod of roughly arm like proportions with a regular dodecagon cross section subject to a head on wind. The rod was covered with materials in accordance with the invention. The principle difference between the trials was the hole sizes used and the angle of the first row of holes with respect to the head-wind. In practice it was found that the angle subtended by the first row of holes into the head wind was not particularly critical. In figure 3 curve 20 shows the test results using a rod coveied with a plain PlastotexTM material without laser holes.
The drag is normalised at 1 for this material at an equivalent wind speed of 1 Om/s (Reynolds Number 70000). As the wind speed increases, following line 20, it can be seen that the drag does not vary much. Looking at lines 22 and 24, which show the results forthe same PlastotexTM material having rows of laser cut holes, the rows being parallel to the axis of the test rod, in accordance with the invention, the drag reduces very sharply above 20 m/s and remains low and constant as speed increases. The difference between curves 22 and 24 is that in the case ot curve 22 the first row of holes was at an angle of 30° to the head wind and in the case of curve 24 it was at 45°. It will be seem that the results show that thealignment of the first row of holes relative to the head wind is not especially sensitive. In both cases the holes themselves were 1.5mm in diameter.
More interesting is the effect of varying the holes. Curve 26 is for a material ha4ng smaller holes (1.25mm) aligned in the same way as curve 22. The impact is large, with the significant drop in drag occurring at a lower Reynolds number (about 1.2*1 0), but the drop is not quite as great as for the larger holes used to produce the curves of 22 and 24. Further rejuctions in hole size down about 1mm moved the position of the drop to the left, just above a Reynolds Number of 0.7*105 but with the lowest drag being higher at 0.7, bigger holes moved the drag reduction to the right, however, the improvement in drag performance was no better than that shown for curves 22 and 24 in figure 3.
The results obtained and in particular the marked reduction of drag are very significant and when applied to a cycling suit result in significant drag reductions at typical speeds reached in racing cycling.
Although the invention has been described in relation to a cycling suit, the principles can be applied to any number of situations. For example a material according to the invention applied to the mast of a yacht would result in reduction of the drag created by the mast.
Claims (26)
- Claims 1. A method of reducing drag on a body in and air stream comprkng the step of covering the object with a material having a ndproof coating thereon and forming one or more elongate bubbles beneath the surface of the windproof coating said elongate bubbles being aligned normally to the direction of the air flow.
- 2. A method according to claim 1 wherein the alignment of elongate bubbles subtends an angle of 70° to 95° to the direction of the air flow.
- 3. A method according to claim 1 or 2 in which the material comprises a windproof coating on a woven material itself over a spacer material
- 4. A method according to claimS in which tie spacer material is between 2 and 4mm inclusive thick.
- 5. A method according to claimS or 4 in which the spacer material is a fleece.
- 6. The method according to any preceding claim in which the windproof coating is polyurethane.
- 7. A method according to any preceding claim in which the material comprises a windproof layer having a plurality of rows of holes through which wind may enter and leave between the windproof layer and the body.
- 8. A method according to claim 7 diaracterised in that the holes between about 1mm and 2mm in diameter.
- 9. A method according to claim 8 diaracterised in that the holes are about 1.5 in diameter.
- 1 0.A method according to claim 7, 8 or 9 characterised in that the holes are in rows, said rows being parallel to an axis of a body on which the material is mounted.
- 11.A method according to any one of claims 7 to 10 Wierein the holes are about 5mm apart.
- 1 2.A method according to any one of claims 7 to 11 in which the holes are laser cut holes.
- 1 3.A material to cover a body or an object or part of such a body or object comprising a spacer layer, a woven layer and a windproof coating applied to the woven layer.
- 14.A material according to claim 13 in which the spacer material is between 2 and 4mm inclusive.
- 15.A material according to claim 13 or 14 in which the spacer material is a fleece.
- 1 6.A material according to claim 13, 14 or 15 in which the wind proof coating is polyurethane.
- 17. A material according to any one of claims 13 to 16 wherein the windproof layer has a plurality of rows of holes through which wind may enter and leave between the windproof layer and the body.
- 1 8.A material according to claim 17 characterised in that the holes between about 1mm and 2mm in diameter.
- 1 9.A material according to claim 18 in which the holes are about 1.5mm in diameter.
- 20.A material according to anyone of claims 17 to 19 charaderised in that the holes are in rows said rows being parallel to an axis of a body on which the material is mounted.
- 21.A material according to any one of claims 17 to2O wherein the holes are about 5mm apart.
- 22.A material according to any one of claims 17 to2l in which the holes are laser cut holes.
- 23.A material according to any one of claims 13 to 22 placed around a body or part thereof and forming a one or more bubbles between the body and the material in an air flow.
- 24.A material according to anyone of claims l3to 23 comprising part of a cyclist's suit.
- 25.A method of reducing drag on a body in an air flow substantially as hereinbefore described with reference to the accompanying drawings.
- 26.A material substantially as hereinbefore described with reference to the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1208081.8A GB2502514A (en) | 2012-05-09 | 2012-05-09 | A drag reduction method and material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1208081.8A GB2502514A (en) | 2012-05-09 | 2012-05-09 | A drag reduction method and material |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201208081D0 GB201208081D0 (en) | 2012-06-20 |
GB2502514A true GB2502514A (en) | 2013-12-04 |
Family
ID=46396722
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1208081.8A Withdrawn GB2502514A (en) | 2012-05-09 | 2012-05-09 | A drag reduction method and material |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2502514A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017108958A1 (en) * | 2015-12-23 | 2017-06-29 | Rheinische Friedrich-Wilhelms Universität Bonn | Grid structures for stable gas retention under liquids |
CN108167282A (en) * | 2017-12-22 | 2018-06-15 | 南京航空航天大学 | A kind of device of reducing friction resistance and the method using its reduction fluid viscous frictional resistance |
US11160318B2 (en) | 2019-12-20 | 2021-11-02 | Joao M P Correla Neves | Wearable airfoil |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2675461A1 (en) * | 1991-04-17 | 1992-10-23 | Julien Pierre | Aerodynamic sail device for propulsion by the wind |
US5887280A (en) * | 1995-03-10 | 1999-03-30 | Waring; John | Wearable article for athlete with vortex generators to reduce form drag |
US20060251859A1 (en) * | 2005-05-05 | 2006-11-09 | D Urso Brian R | Friction drag-reducing surface |
-
2012
- 2012-05-09 GB GB1208081.8A patent/GB2502514A/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2675461A1 (en) * | 1991-04-17 | 1992-10-23 | Julien Pierre | Aerodynamic sail device for propulsion by the wind |
US5887280A (en) * | 1995-03-10 | 1999-03-30 | Waring; John | Wearable article for athlete with vortex generators to reduce form drag |
US20060251859A1 (en) * | 2005-05-05 | 2006-11-09 | D Urso Brian R | Friction drag-reducing surface |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017108958A1 (en) * | 2015-12-23 | 2017-06-29 | Rheinische Friedrich-Wilhelms Universität Bonn | Grid structures for stable gas retention under liquids |
CN108472694A (en) * | 2015-12-23 | 2018-08-31 | 波恩莱茵弗里德里希·威廉大学 | The network retained for stabilizing gas under liquid |
US20180362118A1 (en) * | 2015-12-23 | 2018-12-20 | Rheinische Friedrich-Wilhelms Universität Bonn | Grid structures for stable gas retention under liquids |
CN108167282A (en) * | 2017-12-22 | 2018-06-15 | 南京航空航天大学 | A kind of device of reducing friction resistance and the method using its reduction fluid viscous frictional resistance |
US11160318B2 (en) | 2019-12-20 | 2021-11-02 | Joao M P Correla Neves | Wearable airfoil |
US11382366B2 (en) | 2019-12-20 | 2022-07-12 | Joao M P Correia Neves | Wearable airfoil |
US11771150B2 (en) | 2019-12-20 | 2023-10-03 | Joao M P Correia Neves | Wearable airfoil |
Also Published As
Publication number | Publication date |
---|---|
GB201208081D0 (en) | 2012-06-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |