Air permeability and drag crisis on high tech fabrics for cross country ski competitions.



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Available online at www.sciencedirect.com Procedia Engineering 34 (2012 ) 15 19 9 th Conference of the International Sports Engineering Association (ISEA) Air permeability and drag crisis on high tech fabrics for cross country ski competitions. Luca Oggiano a, Saetran Lars Roar a, Bardal Lars Morten a, Hoying Brian b a Norwegian University of Science and Technology Dept. of Energy and Process Engineering N-7491 Trondheim Norway luca.oggiano@ntnu.no b adidas Group, 5055 N Greeley Ave, Portland, OR, 97217 Accepted 02 March 2012 Abstract The present work aims to investigate possible improvements in cross country ski suits from an aerodynamic perspective with the main goal of evaluating if air permeability plays a significant role in the aerodynamic performances of the textiles. Three different fabrics with different surface pattern and different permeability were tested in a wind tunnel on cylinders with diameter 11cm and 16cm, for speeds ranging from 0-18m/s and with fabric strains from 0-65%. Air permeability tests were also carried out on all the different textiles for the same range of strains. Results show that significant drop in the drag coefficient can been obtained for critical wind speed (V CRIT ) varying between 11m/s and 17m/s depending on textile type and stretch. A clear correlation between air permeability and drag crisis was not found leading to the conclusion that the surface deformation due to the stretching plays a major role if compared with the air permeability. The results obtained show that the lowest V CRIT (11 m/s) achieved in the experiments is above the relevant speeds in cross country skiing (4-9 m/s). 2012 Published by Elsevier Ltd. Keywords: Aerodynamics; textiles; cross coutnry skiing 1. Introduction While sports like speed skating, downhill skiing and cycling [1-8] have been widely analyzed by researchers from an aerodynamic perspective, little focus have been previously put on aerodynamics in cross country skiing. This despite the fact that some authors estimated the influence of drag on total energy expenditure in cross country skiing to vary between 10% and 40%. Thus there might be significant benefits in improving aerodynamics of the athletes in a cross country ski competition [9] 1877-7058 2012 Published by Elsevier Ltd. doi:10.1016/j.proeng.2012.04.004

16 Luca Oggiano et al. / Procedia Engineering 34 ( 2012 ) 15 19 Previous research carried out in textile aerodynamics aims to reduce the drag acting on the athletes by triggering the typical drag crisis that happens on bluff bodies at lower speeds modifying the surface of the textile itself. However, it has not been shown yet that the drag crisis can be triggered to speeds within the range of interest for cross country ski competitions. A closer look at the speed reached by the skiers during the races is then important in order to evaluate if there might be any advantage in using textiles that are able to trigger the drag crisis. To do that, data from the FIS World Cup (WC) of 2010 and 2011 in sprint, 15km, 10 km and marathon races (50-90 km) has been gathered. From the speed analysis the skiing speeds during cross country skiing races was found to vary in a range from 4 to 12m/s where high peak speeds are maintained only for short intervals. During short races, higher speeds were measured (from 5 10m/s) while for longer races like ski marathons the speed varies between 5m/s and 7m/s. Low drag textiles have been in the past investigated by a number of authors and the advantage of using a suit which is able to lower the athletes drag have been shown. Most of the authors [1-6] focused their work on the type of roughness used and how the different types of roughness are able to trigger the transition, some other authors [6, 7, 10]investigated the correlation between air permeability and roughness claiming that the air permeability plays an important role in terms of drag reduction. The present work aims to investigate if there might be sensible improvements in the cross country skiers performances focusing on the improvement of garments worn, and it has the secondary scope to verify if there is a link between air permeability, drag and roughness. 2. Methods 2.1. Wind tunnel test The wind tunnel used for the experiments was the NTNU wind tunnel. The wind tunnel has a crosssection test area of 2.7x1.8 m, with length 11 m and a fan capable of supplying an air velocity of up to 30 m/s. A high resolution 6 component balance produced by Carl Schenk and mounted under the wind tunnel flow was used to acquire the drag. A cylindrical model was built in order to be able to test the different textiles. However, a vertical configuration was chosen instead of a horizontal configuration due to these main reasons: Reduce vibrations by eliminating the arm of the supporting structure Ease the change of PVC-pipe (described later) A more practical approach to obtain an semi-infinite cylinder The test consisted of two parts to allow easy interchangeability of PVC pipes with different diameters. The PVC pipes constitute the outer parts of the rig, upon which the tested materials were placed. The piping had two different diameters (11 cm, 16 cm) that were cut to lengths so that 30 cm was left below and above the cylinders in the wind tunnel. The core of the model was made from a 148 cm long steel tube with an outer diameter 75mm and 3 mm wall thickness that was welded to a 30x20x1cm steel baseplate. The base plate had 10 mm holes drilled in it, spaced 5cm apart to allow mounting it to a 6 component force balance inside the wind tunnel. Combined with the PVC cylinders, the rig had a total height of 150cm. The samples were mounted on cylinders with diameter 11 cm or 16 cm and tested in the wind tunnel at different wind speeds ranging from 4 to 18 m/s. Each sample was tested with five different strain parameters (from 0% to 63%). The fabric were stretched in the weft direction. Five test series with 100 samples per series were collected at each wind speed over a 10 second interval. The highest and lowest measurements were discarded while the three remaining values were averaged. The temperature [T] inside the wind tunnel was measured for each wind speed using a thermometer. The temperatures were then averaged and the air density [ ] together with the air dynamic viscosity [μ] were calculated. Between the testing of each sample, the temperature in the wind tunnel was cooled down to about 22 C.

Luca Oggiano et al. / Procedia Engineering 34 ( 2012 ) 15 19 17 2.2. Air permeability test The air permeability test was performed in the Adidas Laboratories in Portland. The tests were carried out with FX 3320 Mobile Air Permeability Tester from TEXTEST instruments. A custom made four clamps text fixture was built in order to be able to test the air permeability of each textile under the desired stretching. The air permeability was measured for weft-only strain by holding warp strain at 10% strain and stretching from 10% to 70% strain in weft direction. 2.3. Textiles used Three different fabrics with different surface and air permeability characteristics were used in the test. The three textiles (named as T1, T2 and T3) were tested on the cylinder with five different strain values S from a minimum of 0% to a maximum of 63% where the strain value was measured as follows: T1 is a simple knitted textile while dimples of different shapes are present on T2 and T3. T1 and T2 have a simple and smooth surface while T3 has a hairy surface. This is due to the fact that the yarn used in T3 is a textured (spun) yarn while T1 and T2 were assembled with a filament yard Table 1. Textiles used ad structure type. The three textiles used are named T1, T2 and T3 Structure type T1 T2 T3 Yarn type Filament Filament Textured Knit structure Smooth Dimpled Dimpled 3. Results The drag measurements were carried out for all the three samples (T1, T2 and T3) on a 11cm diameter cylinder model and on a 16cm diameter cylinder mode. The samples were stretched with 9%, 23%, 43% and 63%. For the 11cm diameter model test, the results show that, for the range of speed tested (0-16 m/s), the resulting drag coefficient C D varied between 1.1-1.2 showing good agreement with the classic literature [11-15]. T1 and T2 showed a similar behavior, not reaching the transition to turbulent for the range of speed tested while T3 displayed a different behavior showing a significant reduction in C D for speeds higher than 11m/s. This behavior for T3 could be seen for all the different stretch parameters tested with a minimum in C D reaching approximately 0.7. The samples mounted with low strain experienced the transition to turbulence at lower speed than the samples mounted with higher strain. This behavior indicates that the surface distortion caused by the stretching clearly affect the aerodynamic properties. A higher strain smooths the surface of the fabric moving the critical speed closer to the critical speed for a smooth cylinder. For the 16cm diameter cylinder model, all the textiles were able to trip the transition at speeds lower than 16m/s. T1 showed a V CRIT of 15m/s and T2 showed a V CRIT of 13m/s while T3 showed a V CRIT of 11m/s. Fig. 1 summarizes the strain effect on the aerodynamic performance of the textiles by plotting V CRIT against the strain S. The trendline showed in Fig. 1b for the three textiles show that the increase of V CRIT while increaseing the strain is very similar for the three textiles tested.

18 Luca Oggiano et al. / Procedia Engineering 34 ( 2012 ) 15 19 Fig. 1. (a) V CRIT vs. Strain for the 11cm diameter model; (b) V CRIT vs. Strain for the 11cmm diameter model No clear correlation between air permeability and the critical velocity V CRIT was found for any of the samples tested. From the results presented in Fig. 3, a different behavior between the textiles can be noticed. This can be explained by the fact that aerodynamic performances and in thiss case the property of shifting the critical velocity are determined by other factors and air permeability doesn t affect the performances as much as the surface topology does. From Fig. 2, it cann be noticed that the behavior of T2 and T3 are somewhat similar, but not to the extent that there can bee drawn a conclusion based on the influence of the air permeability. Fig. 2 (a) V CRIT vs. Air Permeability for the 16cm diameter model; (b) V CRIT vs. Air Permeability for the 11cm diameter model 4. Conclusions Different fabrics were then to verify the possibility to trip the transition to turbulent regime at a range of speeds interesting for cross country ski competitions (4-9m/s). The fabrics were tested at different strains in order to evaluate the effect of both the surface topography and air permeability on the transition. On the 11 cm cylinder only the T3 sample showed a drag reductionn close to the relevant speed range (11m/s). On the 16cm diameter cylinder, T2 and T1 fabrics showed drag force dropss at around 13 and 15 m/s respectively while the T3 sample experienced a drop at 11 m/s.. The T3 sample therefore has the greatest potential to reduce aerodynamic drag if integrated in cross country skiing suits. However, it is still at the upper limit of the speeds athletes experience during a race.

Luca Oggiano et al. / Procedia Engineering 34 ( 2012 ) 15 19 19 As a major couclusion, in general, the critical speed increases with increasing strain. From the limited data acquired, it can be speculatively noticed that the strain and V CRIT are linearly correlated. However, more data with a larger number of strains are needed to draw a clear conclusion from this point of view. A second finding from our limited amount of data is that the correlation between strain and V CRIT might be independent from the fabric surface, leading to the conclusion that for close fitting garments, surface topography has higher influence than air permeability in the process of shifting the transition to turbulent regime in the boundary layer. Acknowledgements This process has been funded by Adidas and organized by SIAT (Senter for Idrettsanlegg og Teknologi). The Author would like to thank the Adidas Innovation Team for providing materials and samples and for the constant support during the research carried out. References [1] Oggiano L and Sætran L. Effect of different skin suits on speed skating performances. Computer science in sports 3:139 44. [2] Oggiano L and Sætran L. Experimental analysis on parameters affecting drag force on athletes. The impact of Technology on Sport 3:383-9. [3] Oggiano L, Sætran L, Løset S and Winther R. Reducing the athlete s aerodynamical resistance. Journal of computational and applied mechanics 8:163 73. [4] Oggiano L, Troynikov O, Konopov I, Subic A and F. A. Aerodynamic behaviour of single sport jersey fabrics with different roughness and cover factors. Sports Engineering 12:1-12. [5] Brownlie L. Aerodynamic characteristics of sports apparel. School of Kinesiology. [6] Brownlie L, Gartshore M, Mutch B and Banister B. Influence of apparel on aerodynamic drag in running. The Annals of physiological Anthropology 6:133-43. [7] Holden M. The aerodynamic of skiing. The technology of winning 258. [8] Kyle CR and Caiozzo VJ. The effect of athletic clothing aerodynamics upon running speed. Medical Science Journal 18:1299 311. [9] Saibene F. The energy cost of level cross-country skiing and the effect of the friction of the ski. European Journal of Applied Physiology 58:791-5. [10] Watanabe T, Kato T, Kamata Y and Ondera A. The air flow around a clothed cylinder. Seminar i Gakkaishi trans 45:175 82. [11] Achenbach E. Influence of surface roughness on the cross-flow around a circular cylinder. Journal of Fluid Mechanics 46:321-35. [12] Achenbach E. The effect of surface roughness on the heat transfer from a circular cylinder to the cross flow of air. International Journal of Heat and Mass Transfer 20:359 69. [13] Bearman PW and Harvey JK. Control of Circular Cylinder flow by the use of dimples. AIAA-Journal 31:1753 6. [14] Fage A and Warsap GH. The effect of turbulence and surface roughness on the drag of a circular cylinder. [15] Farell C and Fedeniuk SK. Effect of end plates on the flow around rough cylinders. Journal of Wind Engineering and Industrial Aerodynamics 28:219 30.