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Biomechanics and Medicine in Swimming XI

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chaPter2.<strong>Biomechanics</strong><br />

<strong>Biomechanics</strong> <strong>and</strong> <strong>Medic<strong>in</strong>e</strong> <strong>in</strong> Swimm<strong>in</strong>g <strong>XI</strong> Chapter 2 <strong>Biomechanics</strong> b 169<br />

forward unstead<strong>in</strong>ess. This unstead<strong>in</strong>ess permitted to obta<strong>in</strong> a couple<br />

of oppos<strong>in</strong>g forces <strong>and</strong> to <strong>in</strong>fluence the angular momentum. The aim<br />

of this study was to analyze how the start style <strong>in</strong>fluences the angular<br />

stretched upward <strong>and</strong> forward <strong>in</strong>stead of arms) <strong>and</strong> flight start (short block phase but<br />

momentum around the mediolateral axis, as this is an important char-<br />

long flight phase due to great leg power).<br />

acteristic McLean of et the al. start. (2000) calculated the angular momentum of the aerial phase, which is<br />

generated dur<strong>in</strong>g the block phase <strong>in</strong> order to quantify rotation. They analyzed several<br />

Methods<br />

start relay techniques, with <strong>and</strong> without one or two steps before tak<strong>in</strong>g off from the<br />

Five block. elite Tak<strong>in</strong>g male steps front-crawl before leav<strong>in</strong>g spr<strong>in</strong>ters the volunteered block resulted to <strong>in</strong> participate greater takeoff <strong>in</strong> this <strong>and</strong> entry angles<br />

(like a pike start) <strong>and</strong> each step start was characterized by greater body rotation than the<br />

study no-step (22±2 start. years; Pike 180±0.1 trajectory cm; or 74.7±7.9 arm sw<strong>in</strong>g kg; dur<strong>in</strong>g mean the time flight for phase a 100-m (Volkov style) thus<br />

front has crawl an effect <strong>in</strong> a on 50-m body pool: rotation 53.6±1.8 <strong>and</strong> consequently s). Each swimmer on the aerial performed part of the a start. Indeed,<br />

25-m the swim front start crawl cannot three times be reduced at the to 50-m generate race the pace greatest with the forward grab start impulse; the <strong>in</strong>itial<br />

position on is the a blocked block. A forward camera unstead<strong>in</strong>ess. (50 Hz) was This placed unstead<strong>in</strong>ess at the edge permitted of the to obta<strong>in</strong> a<br />

couple of oppos<strong>in</strong>g forces <strong>and</strong> to <strong>in</strong>fluence the angular momentum. The aim of this<br />

pool <strong>and</strong> videotaped the block phase to determ<strong>in</strong>e block phase duration,<br />

study was to analyze how the start style <strong>in</strong>fluences the angular momentum around the<br />

the mediolateral takeoff angle axis, (calculated as this is an from important the centre characteristic of gravity, of the foot start. extremity<br />

<strong>and</strong> horizontal axis), the wrist/shoulder/hip angle (body angle at takeoff<br />

METHODS ), <strong>and</strong> the duration <strong>and</strong> distance of the flight phase. A second camera<br />

(50 Five Hz) elite was male mounted front-crawl on a specially spr<strong>in</strong>ters volunteered designed support to participate placed <strong>in</strong> at this the study lat- (22±2 years;<br />

180±0.1 cm; 74.7±7.9 kg; mean time for a 100-m front crawl <strong>in</strong> a 50-m pool: 53.6±1.8<br />

eral wall 3 m from the edge of the pool deck to videotape the entry phase<br />

s). Each swimmer performed a 25-m front crawl three times at the 50-m race pace with<br />

(entry the grab angle, start calculated position from on the the block. centre A of camera gravity, (50 f<strong>in</strong>ger Hz) was extremity placed <strong>and</strong> at the edge of the<br />

horizontal pool <strong>and</strong> axis videotaped at water the contact). block A phase third to camera determ<strong>in</strong>e (50 block Hz) was phase placed duration, 15 the takeoff<br />

m angle from the (calculated edge of from the pool the centre deck to of determ<strong>in</strong>e gravity, foot the extremity moment the <strong>and</strong> swim- horizontal axis), the<br />

mer’s wrist/shoulder/hip head reached the angle 15-m (body mark angle (placed at takeoff), on the <strong>and</strong> swimm<strong>in</strong>g the duration l<strong>in</strong>e). <strong>and</strong> Im- distance of the<br />

flight phase. A second camera (50 Hz) was mounted on a specially designed support<br />

ages placed were at processed the lateral us<strong>in</strong>g wall Simi-Motion 3 m from the (Simi edge of Reality the pool Motion deck Systems to videotape the entry<br />

GmbH, phase (entry City, angle, Germany). calculated The from spatial the model centre of comprised gravity, f<strong>in</strong>ger 20 anatomical extremity <strong>and</strong> horizontal<br />

l<strong>and</strong>marks axis at water digitalized contact). <strong>in</strong> A each third frame, camera def<strong>in</strong><strong>in</strong>g (50 Hz) a 14-body was placed segment 15 m model from the edge of the<br />

(de pool Leva, deck 1996). to determ<strong>in</strong>e To compute the moment the angular the swimmer’s momentum head for reached each body the seg- 15-m mark (placed<br />

on the swimm<strong>in</strong>g l<strong>in</strong>e). Images were processed us<strong>in</strong>g Simi-Motion (Simi Reality<br />

ment, we evaluated the mechanical parameters such as the segment mass<br />

Motion Systems GmbH, City, Germany). The spatial model comprised 20 anatomical<br />

<strong>and</strong> l<strong>and</strong>marks <strong>in</strong>ertia. For digitalized this purpose, <strong>in</strong> each we frame, assumed def<strong>in</strong><strong>in</strong>g that each a 14-body body segment, segment ex- model (de Leva,<br />

cept 1996). the head, To compute could be the modelled angular momentum as a homogeneous for each cyl<strong>in</strong>der. body segment, The head we evaluated the<br />

was mechanical considered parameters as a sphere. such To obta<strong>in</strong> as the the segment body mass segment <strong>and</strong> <strong>in</strong>ertia, <strong>in</strong>ertia. we For used this purpose, we<br />

the assumed radius of that gyration each body computed segment, by except Zatsiorsky the head, <strong>and</strong> could Seluyanov be modelled (1983). as As a homogeneous<br />

cyl<strong>in</strong>der. The head was considered as a sphere. To obta<strong>in</strong> the body segment <strong>in</strong>ertia, we<br />

the motions were <strong>in</strong> two dimensions, we computed the angular momen-<br />

used the radius of gyration computed by Zatsiorsky <strong>and</strong> Seluyanov (1983). As the<br />

tum motions along the were transverse <strong>in</strong> two dimensions, axis as follows: we computed the angular momentum along the<br />

transverse axis as follows:<br />

i<br />

⎛<br />

L GZ / F * = [ Ii<br />

] wi<br />

z + mi⎜<br />

( GGix<br />

* VGiy<br />

/ F * ) − ( GGi<br />

y * VGix<br />

/ F *<br />

⎝<br />

⎞<br />

)⎟<br />

⎠<br />

where G is the centre of gravity of the whole body, mi is the mass of the ith segment, Gi<br />

where G is the centre of gravity of the whole body, m<br />

is the centre of mass of the ith segment, F* is the barycentric i is the mass of the<br />

frame, Ii is the <strong>in</strong>ertial<br />

i matrix of the ith segment, <strong>and</strong> wi is the angular velocity. The total angular momentum <strong>in</strong><br />

the global frame was then obta<strong>in</strong>ed by add<strong>in</strong>g the local angular momentum of each<br />

segment.<br />

Angular momentum was calculated at takeoff (H, kg.m²/s) <strong>and</strong> the mean st<strong>and</strong>ard<br />

deviation for H (∆H, kg.m²/s) was also calculated. For dynamic analysis, starts were<br />

th segment, Gi is the centre of mass of the results<br />

The takeoff angle differed significantly with the start styles <strong>and</strong> ranged<br />

from 19±3.3° for flat start to 27.8±2.4° for Volkov start (26.8±3.6° was<br />

measured for the pike start). Three swimmers used a flat start def<strong>in</strong>ed<br />

by a low takeoff angle (19±3.3°) <strong>and</strong> one swimmer used the pike start<br />

(26.8±3.6°). The body angle at takeoff (wrist/shoulder/hip) was significantly<br />

different between the three start styles. The Volkov start showed<br />

negative values because of the position of the arms beh<strong>in</strong>d the trunk.<br />

The entry angle was significantly greater for the pike start (34.3±3.9°,<br />

39.7 ±2.8° <strong>and</strong> 37±3.1°, respectively, for the flat, pike <strong>and</strong> Volkov starts).<br />

Although these differences were not statistically significant, greater entry<br />

angles were observed for the pike <strong>and</strong> Volkov vs. the flat start. No<br />

significant difference <strong>in</strong> performance to the 15-m mark was observed<br />

between the start style groups. The takeoff angle, flight distance, <strong>and</strong><br />

the total <strong>and</strong> st<strong>and</strong>ard deviation of the angular momentum were significantly<br />

lower for the flat start than for the two other start styles (with a<br />

significantly longer flight phase for the Volkov start <strong>in</strong> comparison with<br />

the two other starts). The time to 15-m was significantly <strong>and</strong> negatively<br />

correlated with the vertical impulse (r=-0.507) <strong>and</strong> positively correlated<br />

with <strong>Biomechanics</strong> ΔH (r=0.461) <strong>and</strong> <strong>Medic<strong>in</strong>e</strong> (Table <strong>in</strong> Swimm<strong>in</strong>g 1). <strong>XI</strong> Chapter 2 <strong>Biomechanics</strong> b 171<br />

Table 1. Start parameters as a function of start style<br />

Table 1. Start parameters as a function of start style<br />

Start Styles Flat Start (n=3) Pike Start (n=1) Volkov Start (n=2) Correlation<br />

with T15m<br />

Block Phase (s) 0.95±0.04 0.94±0.03 0.89±0.08<br />

Flight Phase (s) 0.26±0.02 0.32±0 a 0.38±0.03 a, b<br />

Flight Distance 3±0.06<br />

(m)<br />

Takeoff Angle 22.1±3.5<br />

(°)<br />

Entry Angle (°) 23.4±2.2<br />

3.2±0.01 a<br />

30.0±2.7 a<br />

24.6±4.8<br />

3.2±0.03 b<br />

34.6±5.2 b<br />

28.2±2.5<br />

Body Angle at<br />

Takeoff (°)<br />

Horizontal<br />

Impulse (N)<br />

Vertical<br />

Impulse (N)<br />

145.3 ±7.6<br />

788.4±48.7<br />

188.7±26.2<br />

27.1±10.5 a<br />

698.9±60.8<br />

171.5±21<br />

- 55.4±13.9 a, b<br />

829.2±61.9 a<br />

205.4±31 r= -0.507<br />

H Takeoff<br />

(kg.m²/s)<br />

∆H (kg.m²/s)<br />

14.7±2.92<br />

0.8±0.13<br />

18.0±0.67 a<br />

1.1±0.2 a<br />

17.5±0.4 b<br />

1.1±0.15 b r= 0.461<br />

Time to 15m (s) 6.5±0.2 6.6±0.08 6.6±0.07<br />

a: significantly different from the previous style on the table; b: significantly different<br />

ith segment, F* is the bary- a: from significantly the flat start different from the previous style on the table; b: significentric<br />

frame, Ii is the <strong>in</strong>ertial matrix of the ith segment, <strong>and</strong> wi is the cantly different from the flat start<br />

DISCUSSION<br />

angular velocity. The total angular momentum <strong>in</strong> the global frame was The aim of this study was to analyze how the start style <strong>in</strong>fluences angular momentum.<br />

then obta<strong>in</strong>ed by add<strong>in</strong>g the local angular momentum of each segment. dIscussIon<br />

The results regard<strong>in</strong>g the k<strong>in</strong>etic momentum showed that significantly less rotation<br />

generated dur<strong>in</strong>g impulsion <strong>in</strong>duced a flat aerial trajectory <strong>and</strong> permitted the swimmers<br />

Angular momentum was calculated at takeoff (H, kg.m²/s) <strong>and</strong> the The to enter aim the of water this more study quickly was (as to demonstrated analyze how by a significantly the start style shorter <strong>in</strong>fluences flight phase). an-<br />

mean st<strong>and</strong>ard deviation for H (ΔH, kg.m²/s) was also calculated. For<br />

dynamic analysis, starts were evaluated with a Bertec 4060-15 force plate<br />

gular The pike momentum. <strong>and</strong> Volkov starts The showed results significantly regard<strong>in</strong>g more the rotation. k<strong>in</strong>etic The momentum arm sw<strong>in</strong>g <strong>in</strong> showed the<br />

pike (forward) <strong>and</strong> Volkov (backward then forward) <strong>in</strong>creased the quantity of rotation.<br />

that In the significantly Volkov start, the less backward rotation sw<strong>in</strong>g generated dur<strong>in</strong>g impulse dur<strong>in</strong>g accelerated impulsion the forward <strong>in</strong>duced rotation a flat<br />

(Bertec Corp., Columbus OH, USA) mounted on a specially built support<br />

fixed to the pool wall to allow a start position that conformed with<br />

the FINA rules. The sampl<strong>in</strong>g rate was 1000 Hz. The analogue signal was<br />

transmitted to a PC through a Biopac A/D converter (Biopac Systems<br />

Inc., Goleta CA, USA). The start signal was <strong>in</strong> accordance with the swimm<strong>in</strong>g<br />

rules <strong>and</strong> was produced by the starter device (ProStart). After filter<strong>in</strong>g<br />

<strong>and</strong> smooth<strong>in</strong>g (Hamm<strong>in</strong>g, low pass, 80 Hz), the reaction time,<br />

impulse time <strong>and</strong> impulse values were obta<strong>in</strong>ed <strong>in</strong> 3D from the force<br />

plate. Only the horizontal <strong>and</strong> vertical axes were analyzed because they<br />

aerial of the body trajectory but the swimmer’s <strong>and</strong> permitted head was <strong>in</strong> the complete swimmers extension, to thus enter <strong>in</strong> opposition the water to the more<br />

arms. The opposite was observed for the pike start. The body angle at takeoff <strong>in</strong>dicated<br />

quickly that the arms (as were demonstrated <strong>in</strong> cont<strong>in</strong>uation by of the a body significantly for the flat style shorter (angle flight close to phase). 180° with The<br />

pike 145.3±7.6°). <strong>and</strong> Volkov The Volkov starts start showed significantly a negative value more due rotation. to the fact The that arm the arms sw<strong>in</strong>g<br />

were beh<strong>in</strong>d the trunk, <strong>and</strong> the values were low for the pike start (27.1±10.5°),<br />

<strong>in</strong> <strong>in</strong>dicat<strong>in</strong>g the pike that (forward) the swimmers <strong>and</strong> were Volkov able (backward to sw<strong>in</strong>g the then arms forward forward) dur<strong>in</strong>g <strong>in</strong>creased the flight the<br />

quantity phase. The of takeoff rotation. <strong>and</strong> entry In angles, the Volkov distance start, to h<strong>and</strong> the entry, backward <strong>and</strong> phase sw<strong>in</strong>g duration dur<strong>in</strong>g were <strong>in</strong> im-<br />

the range of the results provided by the literature: flight distance was 3.09±0.14 m <strong>in</strong><br />

pulse our study accelerated vs. 3.42±0.16 the m for forward McLean rotation et al. (2000), of the <strong>and</strong> the body angular but momentum the swimmer’s was<br />

head 16.2±2.5 was kg.m²/s <strong>in</strong> complete <strong>in</strong> our study extension, vs. 16.4±3.2 thus kg.m²/s <strong>in</strong> opposition for McLean et to al. the (2000). arms. The The<br />

vertical impulse was significantly <strong>and</strong> negatively correlated with time to 15-m,<br />

opposite <strong>in</strong>dicat<strong>in</strong>g that was an observed efficient vertical for the impulse pike needs start. to The be high body enough angle to ensure at takeoff that the <strong>in</strong>dicated<br />

flight distance that is the sufficiently arms were long <strong>in</strong> (this cont<strong>in</strong>uation variable was not of significantly the body for different the among flat style<br />

made up the plane <strong>in</strong> which the swimmer moved. The swimmers’ starts (angle close to 180° with 145.3±7.6°). The Volkov start showed a negative<br />

were classified accord<strong>in</strong>g to the four start styles presented by Seifert et al. value due to the fact that the arms were beh<strong>in</strong>d the trunk, <strong>and</strong> the values<br />

(<strong>in</strong> press). The parameters def<strong>in</strong><strong>in</strong>g the start styles were: block <strong>and</strong> flight were low for the pike start (27.1±10.5°), <strong>in</strong>dicat<strong>in</strong>g that the swimmers<br />

phases, takeoff angle (arms/trunk <strong>and</strong> body/horizontal axes), body angle were able to sw<strong>in</strong>g the arms forward dur<strong>in</strong>g the flight phase. The takeoff<br />

at takeoff (wrist/shoulder/hip), <strong>and</strong> entry angles (body/horizontal axis <strong>and</strong> entry angles, distance to h<strong>and</strong> entry, <strong>and</strong> phase duration were <strong>in</strong><br />

at h<strong>and</strong> entry). After verify<strong>in</strong>g the normality of the data (checked with the range of the results provided by the literature: flight distance was<br />

the Shapiro-Wilk test), ANOVA tests analyzed the variables that signifi- 3.09±0.14 m <strong>in</strong> our study vs. 3.42±0.16 m for McLean et al. (2000), <strong>and</strong><br />

cantly differentiated the start styles. Pearson correlation analysis was also the angular momentum was 16.2±2.5 kg.m²/s <strong>in</strong> our study vs. 16.4±3.2<br />

applied to study the relationships between the start parameters <strong>and</strong> the kg.m²/s for McLean et al. (2000). The vertical impulse was significantly<br />

total 15-m start time (T15m). Statistics were performed with M<strong>in</strong>itab <strong>and</strong> negatively correlated with time to 15-m, <strong>in</strong>dicat<strong>in</strong>g that an effi-<br />

14.10 (M<strong>in</strong>itab Inc., 2003) <strong>and</strong> the level of significance was set at p< 0.05 cient vertical impulse needs to be high enough to ensure that the flight<br />

181

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