Type of variable | Variable | t value | P value |
---|---|---|---|
Flight-related morphology | Body mass (g) | 0.569 | 0.576 |
Wing length (mm) | 16.69 | < 0.001 | |
Wing area (cm2) | 6.158 | < 0.001 | |
Wing loading (N/m2) | 4.326 | < 0.001 | |
Aspect ratio | 5.024 | < 0.001 | |
Load-lifting capacity | Maximum load (g) | 1.321 | 0.202 |
Mass-corrected maximum load | 2.040 | 0.056 | |
Maximum wing loading (N/m2) | 4.326 | < 0.001 | |
Flight kinematics | Wingbeat frequency (Hz) | 6.627 | < 0.001 |
Wing stroke amplitude (deg) | 2.691 | 0.015 | |
Flight performance | Maximum vertical speed (m/s) | 0.625 | 0.540 |
Maximum vertical acceleration (m/s2) | 0.171 | 0.866 | |
Power margin | 0.641 | 0.529 | |
Maximum range speed (Vmr, m/s) | 8.298 | < 0.001 | |
Maximum speed (Vmax, m/s) | 8.176 | < 0.001 | |
Flight energy efficiency | Power at Vmr (W)a | 5.914 | < 0.001 |
Power at Vmax (W) | 6.266 | < 0.001 | |
Mass-corrected power at Vmr (W/kg) | 6.669 | < 0.001 | |
Mass-corrected power at Vmax (W/kg) | 7.228 | < 0.001 | |
Parasitic drag at Vmr (N) | 5.972 | < 0.001 | |
Parasitic drag at Vmax (N) | 5.817 | < 0.001 | |
Reynolds number at Vmr | 3.336 | 0.003 | |
Reynolds number at Vmax | 3.411 | 0.003 | |
Mass-corrected power cost per 100Â km at Vmr (Wh/kg)a | 7.901 | < 0.001 | |
Mass-corrected power cost per 100Â km at Vmax (Wh/kg) | 9.544 | < 0.001 |