Table 2.

Mean values of air density, kinematic, aerodynamic variables in normodense hovering and immediately prior to hypodense hovering failure under both normoxic and hyperoxic conditions

ρ (kg m-3)n (Hz)Φ (°)β (°)ϕmax (°)ϕmin (°)
\({\bar{{\phi}}}\)
(°)
CL,downCL,upRe
Normoxia           
Normodense hovering           
Mean (N=5) 1.14 11.7 112.6 47.0 51.2 -61.4 -5.1 0.82 0.67 37800 
S.D. 0.01 0.9 15.4 2.8 10.5 12.7 8.8 0.23 0.17 7470 
Near-failure           
Mean (N=5) 0.72 11.3 141.6 44.0 61.4 -80.2 -9.4 1.00 0.84 24960 
S.D. 0.04 0.97 16.9 4.0 12.5 8.2 6.4 0.47 0.33 4490 
Hyperoxia           
Normodense hovering           
Mean (N=3) 1.13 11.3 108.8 51.4 46.7 -62.1 -7.7 0.76 0.63 38150 
S.D. 0.00 0.48 19.0 6.9 11.6 12.0 7.0 0.20 0.15 5710 
Near-failure           
Mean (N=3) 0.70 11.2 138.0 49.2 55.6 -82.4 -13.4 0.74 0.64 32600 
S.D. 0.06 0.78 18.0 7.8 11.3 10.3 5.9 0.28 0.23 11370 
ρ (kg m-3)n (Hz)Φ (°)β (°)ϕmax (°)ϕmin (°)
\({\bar{{\phi}}}\)
(°)
CL,downCL,upRe
Normoxia           
Normodense hovering           
Mean (N=5) 1.14 11.7 112.6 47.0 51.2 -61.4 -5.1 0.82 0.67 37800 
S.D. 0.01 0.9 15.4 2.8 10.5 12.7 8.8 0.23 0.17 7470 
Near-failure           
Mean (N=5) 0.72 11.3 141.6 44.0 61.4 -80.2 -9.4 1.00 0.84 24960 
S.D. 0.04 0.97 16.9 4.0 12.5 8.2 6.4 0.47 0.33 4490 
Hyperoxia           
Normodense hovering           
Mean (N=3) 1.13 11.3 108.8 51.4 46.7 -62.1 -7.7 0.76 0.63 38150 
S.D. 0.00 0.48 19.0 6.9 11.6 12.0 7.0 0.20 0.15 5710 
Near-failure           
Mean (N=3) 0.70 11.2 138.0 49.2 55.6 -82.4 -13.4 0.74 0.64 32600 
S.D. 0.06 0.78 18.0 7.8 11.3 10.3 5.9 0.28 0.23 11370 

Abbreviations: n, wingbeat frequency; Φ, stroke amplitude;β, stroke plane angle; ϕmax, maximum wing positional angle; ϕmin, minimum wing positional angle;

\({\bar{{\phi}}}\)
⁠, mean positional angle; CL,down, mean lift coefficient during downstroke; CL,up, mean lift coefficient during upstroke; Re,mean Reynolds number.

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