Biomechanics and Medicine in Swimming XI
Biomechanics and Medicine in Swimming XI
Biomechanics and Medicine in Swimming XI
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The Effect of Angle of Attack <strong>and</strong> Depth on Passive<br />
Drag<br />
Pease, d.l. 1 , Vennell, r. 2<br />
1 Australian Institute of Sport, Canberra, Australia<br />
2 University of Otago, Duned<strong>in</strong>, New Zeal<strong>and</strong><br />
In order to quantify the effect of angle of attack <strong>and</strong> depth on drag force<br />
dur<strong>in</strong>g underwater glid<strong>in</strong>g the current study was undertaken. This aim<br />
was achieved by utilis<strong>in</strong>g a flume <strong>and</strong> an anatomically accurate mannequ<strong>in</strong><br />
whose orientation could be precisely controlled. Measurements<br />
were obta<strong>in</strong>ed with the mannequ<strong>in</strong> oriented with the longitud<strong>in</strong>al axis<br />
at angles of attack of -4, -2, 0, +2 <strong>and</strong> +4 degrees relative to water flow.<br />
Measurements were taken at depths rang<strong>in</strong>g from 0.2 – 0.8m <strong>and</strong> at<br />
velocities rang<strong>in</strong>g from 0-2.55ms -1 . There was generally little effect<br />
from the angle of attack other than near the surface (0.2m) where<br />
there was a tendency for the wave drag to be lower for the negative<br />
angles. This f<strong>in</strong>d<strong>in</strong>g <strong>in</strong>dicates that as swimmers approach<br />
the surface it may be beneficial to adopt a slight negative angle of<br />
attack <strong>in</strong> order to m<strong>in</strong>imise the drag force.<br />
Key words: swimm<strong>in</strong>g, passive drag, wave drag, angle of attack, flume<br />
IntroductIon<br />
Previous research <strong>in</strong>to the drag forces (both active <strong>and</strong> passive) act<strong>in</strong>g<br />
dur<strong>in</strong>g human swimm<strong>in</strong>g has shown differences due to body size, shape,<br />
velocity <strong>and</strong> depth. However, one factor, which has not previously been<br />
<strong>in</strong>vestigated, is that of the angle of attack or pitch angle of the athlete’s<br />
body relative to the water flow. Angle of attack is a factor, which has<br />
been highlighted as an issue <strong>in</strong> previous study but due to the <strong>in</strong>ability<br />
to systematically control this factor it has been generally described as a<br />
limitation.<br />
Therefore, the present study was undertaken to try <strong>and</strong> quantify the effect<br />
of angle of attack on the drag forces act<strong>in</strong>g upon a streaml<strong>in</strong>ed human<br />
swimmer by utilis<strong>in</strong>g an anatomically accurate mannequ<strong>in</strong> whose orientation<br />
relative to the water flow direction could be precisely controlled.<br />
It was hypothesized that, as angle of attack changed, there would<br />
be significant changes <strong>in</strong> the magnitude of the total drag force as well<br />
as changes <strong>in</strong> the relative contribution of the component forces, viscous,<br />
form, <strong>and</strong> wave drag. These changes would be primarily due to the<br />
changes <strong>in</strong> exposed frontal area with <strong>in</strong>creas<strong>in</strong>g (positive <strong>and</strong> negative)<br />
angles of attack away from the zero angle.<br />
Based on the f<strong>in</strong>d<strong>in</strong>gs from previous research (Vennell, Pease, &<br />
Wilson, 2006) there are <strong>in</strong>creases <strong>in</strong> the total drag force, <strong>and</strong> more specifically<br />
the wave drag contribution to that total force, as depth of the<br />
swimmer decreases. Therefore, another aspect of the current study was<br />
to exam<strong>in</strong>e the <strong>in</strong>teraction between angle of attack <strong>and</strong> submergence<br />
depth <strong>and</strong> the measured drag force.<br />
Previous studies have quantified body angles similar to angle of attack<br />
dur<strong>in</strong>g free surface swimm<strong>in</strong>g (Zamparo, 2006; Zamparo et al.,<br />
2008) with the aim of us<strong>in</strong>g that angle as an <strong>in</strong>dicator of body position.<br />
In general the angle of the trunk to the horizontal is used to represent<br />
angle of attack. In those studies body angles of approximately 15 degrees<br />
were found. However, dur<strong>in</strong>g the streaml<strong>in</strong>ed portion of a swimm<strong>in</strong>g<br />
race when the athlete is fully submerged, <strong>and</strong> not mov<strong>in</strong>g on a<br />
fluid boundary, it was theorised that the angle of attack would be much<br />
less due to the freedom of the athlete’s body to move <strong>in</strong> the vertical as<br />
well as the horizontal plane. This is unlike surface swimm<strong>in</strong>g where the<br />
movement trajectory is fixed <strong>and</strong> essentially limited to the horizontal<br />
plane. By allow<strong>in</strong>g for movement <strong>in</strong> the vertical plane as well as the<br />
horizontal, the trajectory of the centre of mass is more <strong>in</strong> l<strong>in</strong>e with the<br />
angle of the body thereby reduc<strong>in</strong>g the angle of attack relative to the<br />
surround<strong>in</strong>g water flow.<br />
chaPter2.<strong>Biomechanics</strong><br />
Therefore, the current study exam<strong>in</strong>ed smaller angles of attack which<br />
may be achieved by fully submerged swimmers <strong>in</strong> a streaml<strong>in</strong>e position<br />
such as that experienced follow<strong>in</strong>g starts <strong>and</strong> turns.<br />
Methods<br />
All test<strong>in</strong>g was conducted <strong>in</strong> the aquatic treadmill or ’flume’ at the University<br />
of Otago, as described by Britton, Rogers, <strong>and</strong> Reimann (1998).<br />
In order to achieve the desired control over position of the body<br />
relative to water flow it was necessary to utilise an anatomically accurate<br />
mannequ<strong>in</strong> rather than live subjects. The mannequ<strong>in</strong> used was the<br />
same as that described <strong>in</strong> previous research (Bixler & Pease, 2006; Bixler,<br />
Pease, & Fairhurst, 2007; Vennell et al., 2006) <strong>and</strong> had a total surface<br />
area of 1.859m 2 which allowed for the determ<strong>in</strong>ation of an estimate for<br />
viscous frictional force.<br />
The mount<strong>in</strong>g structure used to support the mannequ<strong>in</strong> was similar<br />
to that used <strong>in</strong> the previous studies. However, <strong>in</strong> the previous work the<br />
mannequ<strong>in</strong> was mounted via a tow<strong>in</strong>g arrangement through the f<strong>in</strong>gertips,<br />
which allowed for free movement of the rest of the mannequ<strong>in</strong>’s<br />
body. Therefore a new mount<strong>in</strong>g was necessary which allowed for the<br />
ma<strong>in</strong>tenance of orientation at all times. In the modified structure the<br />
mannequ<strong>in</strong> is fixed directly to a vertical aerofoil spar, which is attached<br />
at the back of the mannequ<strong>in</strong>. This aerofoil spar is then bolted to the<br />
same vertical pole <strong>and</strong> mount<strong>in</strong>g structure described by Vennell et al.<br />
(2006). The vertical spar is <strong>in</strong>f<strong>in</strong>itely adjustable <strong>in</strong> terms of mannequ<strong>in</strong><br />
depth between 0 <strong>and</strong> 0.9m. However, for the purposes of the current<br />
study the depths utilised were 0.2 – 0.8m at 0.1m <strong>in</strong>crements. Depth<br />
was measured as the distance between the water free surface <strong>and</strong> the<br />
central longitud<strong>in</strong>al axis of the mannequ<strong>in</strong>.<br />
The vertical pole then was clamped to a horizontally oriented triaxial<br />
load cell, AMTI model MC3-6-1000, with the Z axis parallel to<br />
the water flow direction. The load cell was <strong>in</strong> turn <strong>in</strong>terfaced with an<br />
AMTI MCA6 amplifier <strong>and</strong> f<strong>in</strong>ally to a PowerLab unit which allowed<br />
for cont<strong>in</strong>uous data collection. Vertical position of the mannequ<strong>in</strong>s was<br />
controlled by rais<strong>in</strong>g or lower<strong>in</strong>g the vertical spar <strong>and</strong> pole. The position<br />
was then fixed by a set screw at the gimbal, <strong>and</strong> a scaffold<strong>in</strong>g clamp attached<br />
<strong>in</strong> series with the tri-axial load cell.<br />
In order to obta<strong>in</strong> the optimal drag-velocity curves for the mannequ<strong>in</strong>,<br />
data was collected for 13 velocities: 0, 0.34, 0.55, 0.75, 0.95, 1.16,<br />
1.36, 1.57, 1.77, 1.94, 2.15, 2.36, <strong>and</strong> 2.55 ms -1 respectively at each of<br />
the tow depths described previously. These conditions were repeated for<br />
each of the angles of attack; -4, -2, 0, +2, <strong>and</strong> +4° respectively. Angles of<br />
attack were based on a 0° orientation def<strong>in</strong>ed as that position with the<br />
m<strong>in</strong>imum projected frontal cross sectional area. Six tests of five seconds<br />
<strong>in</strong> duration were undertaken for each test condition.<br />
The projected frontal areas for these tested angles of attack were:<br />
0.1282, 0.1156, 0.1079, 0.1124, <strong>and</strong> 0.1280m 2 respectively. While attack<br />
angles greater than those tested may be exhibited <strong>in</strong> real situations,<br />
due to the uncerta<strong>in</strong>ty of the magnitude of load changes beyond the<br />
angles measured, limits were set <strong>in</strong> order to m<strong>in</strong>imise the possibility of<br />
damag<strong>in</strong>g either the mannequ<strong>in</strong> or the test<strong>in</strong>g support structure. Secondly,<br />
if angles greater than those tested had been utilised there would<br />
have been protrusion of the mannequ<strong>in</strong> through the water surface at<br />
the m<strong>in</strong>imum depth, which would have changed the wetted area <strong>and</strong><br />
thereby affected the results.<br />
In order to detect any effects of angle of attack on the drag forces,<br />
correlation coefficients were determ<strong>in</strong>ed between the angles of attack<br />
<strong>and</strong> the respective drag force components. In order to utilise correlational<br />
analyses a l<strong>in</strong>ear relationship between angle of attack <strong>and</strong> drag was<br />
hypothesized due to the l<strong>in</strong>early decreas<strong>in</strong>g depth of the lead<strong>in</strong>g edge<br />
of the mannequ<strong>in</strong>. Dur<strong>in</strong>g the pilot test<strong>in</strong>g the data were analysed for<br />
normality of distribution <strong>and</strong> were deemed to be suitable for parametric<br />
analysis. Due to the limitation of only utilis<strong>in</strong>g the s<strong>in</strong>gle mannequ<strong>in</strong><br />
the magnitude of the correlation coefficient needed to be very high <strong>in</strong><br />
order to achieve statistical significance (r≥.858 for significance at the 0.1<br />
level <strong>and</strong> r≥.959 for significance at the .05 level)<br />
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