| Literature DB >> 36009850 |
Pau Cecília-Gallego1,2, Adrián Odriozola3,4,5, José Vicente Beltrán-Garrido1,6, Jesús Álvarez-Herms3,4,5.
Abstract
Overspeed is a training method used to improve running speed, although its effects are not supported by consensual scientific evidence. The overspeed stimulus can be boosted by several methods, including motorized towing devices. Our objectives were to analyze the acute effects of three overspeed loads in young athletes and to select optimal loads for training periods. Eight young athletes (16.73 ± 1.69 years) performed one unassisted sprint and three assisted sprints, and kinematic and biomechanical data were compared. Significant increases (p < 0.05) in step velocity and step length were found with 2, 4, and 5.25 kg in maximum running speed, flight time and horizontal distance from the first contact to the vertical projection of the center of mass with 4 and 5.25 kg. Significant time decreases were found in 5 m flying sprint and contact time with 4 and 5.25 kg, and no significant changes were observed in step rate. The individually recommended loads would be between 3.47 ± 0.68% and 6.94 ± 1.35% body weight. Even having limitations, we can understand this work and its results as a pilot study to replicate the methodology and the use of new devices to more broadly investigate the effects of overspeed.Entities:
Keywords: amateur athletes; assisted sprint; body weight; ecological approach; individualization
Year: 2022 PMID: 36009850 PMCID: PMC9405254 DOI: 10.3390/biology11081223
Source DB: PubMed Journal: Biology (Basel) ISSN: 2079-7737
Characteristics of the participants and % of body weight in assistance loads.
| Sex | Males (3) | Females (5) | All (8) |
|---|---|---|---|
| Age (years) | 15.98 ± 1.09 | 17.18 ± 1.57 | 16.73 ± 1.69 |
| Years from PHV | 2.13 ± 0.68 | 3.96 ± 1.39 | 3.28 ± 1.46 |
| Years of training | 5.33 ± 1.15 | 5.60 ± 1.34 | 5.50 ± 1.20 |
| Height (cm) | 174.87 ± 5.78 | 160.72 ± 13.81 | 166.03 ± 10.56 |
| Weight (kg) | 63.22 ± 2.86 | 56.62 ± 10.53 | 59.09 ± 8.70 |
| Fat mass % | 7.50 ± 0.17 | 16.18 ± 6.54 | 12.93 ± 5.62 |
| % BW OS1 | 3.17 ± 0.14 | 3.65 ± 0.84 | 3.47 ± 0.68 |
| % BW OS2 | 6.34 ± 0.29 | 7.31 ± 1.68 | 6.94 ± 1.35 |
| % BW OS3 | 8.71 ± 0.40 | 9.28 ± 1.81 | 9.07 ± 1.52 |
| PB 60 m (s) | 7.63 ± 0.06 | 8.32 ± 0.60 | 8.06 ± 0.47 |
Data are shown as average ± SD. PHV: peak height velocity; BW: body weight; OS: overspeed load (1: 2 kg; 2: 4 kg; 3: 5.25 kg); PB: personal best in 60 m dash with automatic timing.
Kinematic parameters of the different speed conditions.
| Variable | S0 | O1 | OS2 | OS3 | ANOVA |
|
|---|---|---|---|---|---|---|
| T5m (s) | 0.61 ± 0.04 | 0.59 ± 0.04 | 0.58 ± 0.03 * L | 0.56 ± 0.05 * VL # L | <0.001 | 0.72 L |
| V5m (m/s) | 8.23 ± 0.58 | 8.46 ± 0.57 | 8.62 ± 0.48 * L | 8.92 ± 0.70 * VL # L ^ M | <0.001 | 0.71 L |
| SV (m/s) | 8.59 ± 0.74 | 8.88 ± 0.65 * L | 9.06 ± 0.71 * L | 9.43 ± 0.73 * VL # L ^ L | <0.001 | 0.78 L |
| SR (step/s) | 4.31 ± 0.25 | 4.30 ± 0.26 | 4.27 ± 0.28 | 4.31 ± 0.26 | 0.753 | 0.05 S |
| SL (cm) | 199.34 ± 12.36 | 206.97 ± 13.96 * M | 212.70 ± 15.44 * L | 219.12 ± 13.75* VL # L | <0.001 | 0.75 L |
| FT (s) | 0.119 ± 0.014 | 0.124 ± 0.014 | 0.127 ± 0.017 * L | 0.125 ± 0.012 * S | 0.003 | 0.47 L |
| CT (s) | 0.114 ± 0.010 | 0.110 ± 0.007 | 0.109 ± 0.010 * M | 0.108 ± 0.009 * L | 0.009 | 0.41 L |
| HD (cm) | 34.16 ± 4.06 | 35.60 ± 3.67 | 38.48 ± 3.81 * VL # VL | 39.72 ± 4.16 * VL # VL | <0.001 | 0.74 L |
Values are presented as average ± SD. S0: speed without assistance load; OS: assistance loads (1: 2 kg; 2: 4 kg; 3: 5.25 kg); T5m: time between meters 40 and 45 with a flying start; V5m: speed between meters 40 and 45 with a flying start; SV: step velocity between meters 42.5 and 47.5 with a flying start; SR: step rate; SL: step length; FT: flight time; CT: contact time; HD: horizontal distance between the point of first contact with the ground and the vertical projection of the center of mass; * p ≤ 0.05 different from the S0 condition; # p ≤ 0.05 different from the OS1 condition; ^ p ≤ 0.05 different from the OS2 condition; T: trivial effect size; S: small effect size; M: medium/moderate effect size; L: large effect size; VL: very large effect size; 2p: partial squared eta effect size.
Percentages of change of each condition with respect to S0.
| Variables | OS 1–S0 | OS 2–S0 | OS 3–S0 |
|---|---|---|---|
| T5m | −4.80 ± 6.29 | −6.64 ± 5.41 | −9.55 ± 7.36 |
| V5m | +2.91 ± 2.91 | +4.88 ± 3.01 | +8.42 ± 3.48 |
| SV | +3.46 ± 2.73 | +5.62 ± 3.47 | +9.84 ± 3.30 |
| SR | −0.32 ± 2.39 | −0.94 ± 3.08 | −0.09 ± 1.76 |
| SL | +3.83 ± 2.36 | +6.70 ± 4.30 | +9.95 ± 3.24 |
| FT | +4.12 ± 2.30 | +6.12 ± 4.91 | +5.36 ± 3.18 |
| CT | −3.23 ± 3.23 | −4.41 ± 3.47 | −4.47 ± 3.76 |
| HD | +4.59 ± 6.93 | +13.20 ± 10.18 | +16.62 ± 7.30 |
The values are expressed as the % change of each condition with respect to S0. S0: without assistance load; OS: assistance loads (1: 2 kg; 2: 4 kg; 3: 5.25 kg); T5m: time between meters 40 and 45 with a flying start; V5m: speed between meters 40 and 45 with a flying start; SV: step velocity between meters 42.5 and 47.5 with a flying start; SR: step rate; SL: step length; FT: flight time; CT: contact time; HD: horizontal distance between the point of first contact with the ground and the vertical projection of the center of mass.
Figure 1Individual percentages of change for the variables (A) V5m, (B) SL and (C) HD in the different experimental conditions. The gray shaded area highlights the percentage change range between 3% and 5%. V5m: speed between meters 40 and 45 with a flying start; SL: step length; HD: horizontal distance between the point of first contact with the ground and the vertical projection of the center of mass.