| Literature DB >> 17645390 |
Thomas Alerstam1, Mikael Rosén, Johan Bäckman, Per G P Ericson, Olof Hellgren.
Abstract
Flight speed is expected to increase with mass and wing loading among flying animals and aircraft for fundamental aerodynamic reasons. Assuming geometrical and dynamical similarity, cruising flight speed is predicted to vary as (body mass)(1/6) and (wing loading)(1/2) among bird species. To test these scaling rules and the general importance of mass and wing loading for bird flight speeds, we used tracking radar to measure flapping flight speeds of individuals or flocks of migrating birds visually identified to species as well as their altitude and winds at the altitudes where the birds were flying. Equivalent airspeeds (airspeeds corrected to sea level air density, Ue) of 138 species, ranging 0.01-10 kg in mass, were analysed in relation to biometry and phylogeny. Scaling exponents in relation to mass and wing loading were significantly smaller than predicted (about 0.12 and 0.32, respectively, with similar results for analyses based on species and independent phylogenetic contrasts). These low scaling exponents may be the result of evolutionary restrictions on bird flight-speed range, counteracting too slow flight speeds among species with low wing loading and too fast speeds among species with high wing loading. This compression of speed range is partly attained through geometric differences, with aspect ratio showing a positive relationship with body mass and wing loading, but additional factors are required to fully explain the small scaling exponent of Ue in relation to wing loading. Furthermore, mass and wing loading accounted for only a limited proportion of the variation in Ue. Phylogeny was a powerful factor, in combination with wing loading, to account for the variation in Ue. These results demonstrate that functional flight adaptations and constraints associated with different evolutionary lineages have an important influence on cruising flapping flight speed that goes beyond the general aerodynamic scaling effects of mass and wing loading.Entities:
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Year: 2007 PMID: 17645390 PMCID: PMC1914071 DOI: 10.1371/journal.pbio.0050197
Source DB: PubMed Journal: PLoS Biol ISSN: 1544-9173 Impact factor: 8.029
Figure 1Bird Flight Speeds (U e; m/s) Plotted in Relation to Body Mass (kg) and Wing Loading (N/m2) for 138 Species of Six Main Monophyletic Groups
The lines show the scaling relationships U e = 15.9 × (mass)0.13 and U e = 4.3 × (wing loading)0.31 as calculated by reduced major axis regression for all species (Table 1). All axes are in logarithmic scale. Inserts show means (± standard deviations) for the six main phylogenetic groups in relation to these scaling lines. Species of the same group tend to fly at similar speeds, and phylogenetic group is an important factor to account for the variation in U e.
Allometric Relationships between Bird Flight Speed (U e; m/s) and Body Mass (kg) and between U e and Wing Loading (N/m2)
Figure 2Explanation of the Variation in Mean Flight Speeds (U e; m/s) among Bird Species by Different Combinations of Variables and Factors
The explanatory power (adjusted R 2) of different General Linear Models with significant independent variables (***, p < 0.001) is illustrated. Phylogenetic group and wing loading emerge as key factors to account for the variation in flight speed among bird species. General Linear Models for all different combinations of body mass, wing loading, aspect ratio, and phylogenetic group were calculated, except combinations including both body mass and wing loading (because of the interdependence between these variables). Complex models (including combinations of variables) are presented only if the AIC improved from models based on single independent variables [17]. This applied only to the model incorporating both phylogenetic group and wing loading. ΔAIC indicates the difference in AIC score from the most effective model (with ΔAIC = 0). Test statistics were as follows (in parentheses) for model including mass (F 1,136 = 20.0, p < 0.001), aspect ratio (F 1,127 = 28.6, p < 0.001), wing loading (F 1,127 = 122.6, p < 0.001), phylogenetic group (F 5,132 = 34.5), and phylogenetic group plus wing loading (F 6,122 = 39.6, p < 0.001).