F(2,15)=3.877 | F(2,15)= 9.019 | F(2,15)=21.043 | ||||
p=0.044 | p=0.003 | p=0.0001 | ||||
p=0.003 | p=0.0001 | |||||
p=0.014 | p=0.001 | p=0.0001 | ||||
F(2,16)=12.566 | F(2,16)=18.46 | F(2,16)=4.948 | F(2,16)=15.68 | |||
p=0.001 | p=0.0001 | p=0.021 | p=0.0001 | |||
p=0.0001 | p=0.002 | p=0.019 | p=0.0001 | |||
p=0.001 | p=0.0001 | p=0.009 | p=0.0001 | |||
F(2,16)=27.176 | F(2,16)=5.839 | F(2,16)=5.723 | F(2,16)=23.897 | |||
p=0.0001 | p=0.012 | p=0.013 | p=0.0001 | |||
p=0.0001 | p=0.006 | p=0.007 | p=0.030 | p=0.0001 | ||
p=0.0001 | p=0.012 | p=0.010 | p=0.043 | p=0.0001 | ||
F(2,15)=7.660 | F(2,15)=9.843 | |||||
p=0.005 | p=0.002 | |||||
p=0.002 | p=0.017 | p=0.033 | p=0.001 | |||
p=0.005 | p=0.042 | p=0.008 | ||||
F(2,10)=5.381 | F(2,10)=8.331 | |||||
p=0.026 | p=0.007 | |||||
p=0.016 | p=0.005 | |||||
p=0.024 | p=0.008 | |||||
F(2,16)=11.626 | F(2,16)=9.947 | F(2,16)=17.750 | ||||
p=0.001 | p=0.002 | p=0.0001 | ||||
p=0.001 | p=0.001 | p=0.0001 | ||||
p=0.0001 | p=0.046 | p=0.002 | p=0.046 | p=0.0001 |
Day | Group | Ankle angle (deg) | Knee angle (deg) | ||
---|---|---|---|---|---|
Maximum | Minimum | Maximum | Minimum | ||
(most extended) | (most flexed) | (most extended) | (most flexed) | ||
R0 | Flight | 151±8.8 (3) | 40±3.8 (3) | 118±7.1 (3) | 43±6.7 (3) |
Control | 138±1.6 (5) | 50±4.5 (5) | 121±6.5 (5) | 49±2.1 (5) | |
R1 | Flight | 153±5.7 (3) | 62±13.1 (3) | 96±0.5 (3) | 34±3.7 (3) |
Control | 139±1.8 (3) | 65± 5.5 (3) | 106±6.3 (3) | 47±3.2 (3) | |
R7 | Flight | 134±2.1 | 53±3.4 (5) | 121±3.6 (5) | 68±7.5 (5) |
Control | 123±1.4 (4) | 54±5.4 (4) | 122±1.8 (4) | 77±5.5 (4) | |
R14 | Flight | 133±3.7 (6) | 52±1.1 (6) | 116±2.1 (6) | 63±8.8 (6) |
Control | 124±4.4 (4) | 57±3.3 (4) | 123±4.4 (4) | 73±6.9 (4) |
R0 | t(17)=5.731 | t(9)=−3.199 | t(9)= −2.358 | t(9)= −3.35 | |
p=0.0001 | p=0.011 | p=0.043 | p=0.005 | ||
R1 | t(16)=4.289 | t(16)= −3.026 | t(8)= −2.986 | ||
p=0.001 | p=0.008 | p=0.01 | |||
R2 | t(16)=5.394 | t(16)= −2.724 | t(16)= −2.6 | ||
p=0.0001 | p=0.015 | p=0.019 | |||
R3 | t(16)=3.734 | t(16)= −3.438 | |||
p=0.002 | p=0.003 | ||||
R4 | t(15)=2.745 | t(15)= −2.155 | |||
p=0.015 | p=0.048 | ||||
R5 | t(9.8)=2.557 | t(8.5)= −3.089 | |||
p=00.029 | p=0.014 | ||||
R6 | t(9.2)=2.363 | ||||
p=0.042 |
75.4± 9.5 | 5.6± 3.9 | 16.8±8.5 | 0 | 0 | 100 | ||
91.3± 4.5 | 8.7± 4.5 | 0 | 0 | 0 | 100 | ||
14.5± 6.6 | 7.5± 4.8 | 35.3±8.0 | 11.4±5.9 | 31.31±15.3 | 100 | ||
85.6±10.9 | 11.1±11.1 | 3.3±3.3 | 0 | 0 | 100 |
Posture | Group | Mean (ms) | Standard error of the mean (ms) | n |
---|---|---|---|---|
Axial | Basal | 972 | 68 | 7 |
Control | 163 | 4 | 16 | |
Flight | 192 | 13 | 6 | |
Corkscrew | Basal | 1323 | 74 | 7 |
Control | 202 | 10 | 10 | |
Flight | 237 | 27 | 4 | |
L-posture | Basal | — | — | 0 |
Control | 665 | 14 | 4 | |
Flight | 422 | 38 | 2 | |
U-posture | Basal | 899 | 51 | 6 |
Control | 250 | 14 | 6 | |
Flight | 258 | 20 | 4 | |
U and C | Basal | 1213 | 95 | 6 |
Control | 240 | 8 | 3 | |
Flight | 349 | 78 | 4 |