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First published online October 7, 2008
Journal of Experimental Biology 211, 3205-3213 (2008)
Published by The Company of Biologists 2008
doi: 10.1242/jeb.012468
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Ontogenetic changes in the structural stiffness of the tailstock of bottlenose dolphins (Tursiops truncatus)

S. A. Etnier1,*, W. A. McLellan2, J. Blum3 and D. A. Pabst2

1 Department of Biological Sciences, Butler University, Indianapolis, IN 46208, USA
2 Biology and Marine Biology, University of North Carolina Wilmington, Wilmington, NC 28403, USA
3 Mathematics and Statistics, University of North Carolina Wilmington, Wilmington, NC 28403, USA


Figure 1
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Fig. 1. En utero position of a fetal dolphin (PTM 114f, total length 81 cm). The dorsal fin and tail flukes are still floppy, with the flukes juxtaposed to the chin. Note the presence of prominent fetal folds. The scale bar is 15.8 cm in length.

 

Figure 2
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Fig. 2. (A) Schematic drawing of the bending apparatus used for determining structural stiffness (EI, Nm2). The thick gray line represents the central axis of the animal and the triangle at the bottom of the image represents the flukes. (B) Actual image of the bending apparatus as seen from above. The specimen shown here is a Grampus griseus (WAM 570, total length 215 cm), positioned for lateral deformations. The animal is immobilized with two ratchet tie-downs cranial and caudal to the pectoral fin. The central axis of the animal is marked with zinc oxide dots, while the center of the dorsal fin, the anus and the mid-peduncle are marked with horizontal white lines.

 

Figure 3
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Fig. 3. Representative diagrams showing dorsoventral and lateral deformations of the caudal tailstock of one individual from each of the different life-history stages under various loads. The vertical line represents the center of the dorsal fin and the head is pointing to the right in all images. The lines showing deformation of the tailstock depict the central axis of the animal, as determined by positions 2, 4, 6 and 8 as described in Materials and methods. The direction and applied load are listed next to the resultant deformation, while the neutral line shows the posture of the animal with no applied load. (A) Dorsal view of lateral deformation for loads ranging from 0 to 49 N. In the fetus, bending to the right occurred freely, with no applied load (R no load), while maximum deformation (R max. load) occurred with the application of a load too small to be quantified by our apparatus. (B) Lateral view of dorsoventral deformations for loads ranging from 0 to 66.6 N. Note that the images are not to scale. L, left; R, right; D, dorsal; V, ventral; TL, total body length (cm).

 

Figure 4
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Fig. 4. Overall curvature (m–1) for an ontogenetic series of dolphins when deformed with a maximal load. Values are shown for deformation in the lateral (mean value for both left and right), dorsal and ventral directions. The maximal load is the point at which any increased load resulted in no further deformation or caused unnatural distortion of the body. Vertical dotted lines distinguish different life-history stages.

 

Figure 5
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Fig. 5. Structural stiffness and stiffness constants for an ontogenetic series of dolphins. Values are shown for deformation in the lateral (mean value for both left and right), dorsal and ventral directions. Vertical dotted lines distinguish different life-history stages. (A) Structural stiffness was calculated for deformations that were less than 10% of total body length and thus often represent single data points. For dorsal and ventral deformations, the average standard deviation was 7.5 and 0.8, respectively. For lateral deformations, the average standard deviation was 9.8. Fetal deformations typically exceeded the stated criterion, even with loads that were too small to be measured with our apparatus. For these animals, we assumed a load of 0.98 N and used the resultant deformations. Thus, these values should be considered approximations. (B) Stiffness constant (k) for an ontogenetic series of dolphins. Values were calculated for all deformations that exceeded 10% of total body length.

 

Figure 6
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Fig. 6. (A) The neutral zone for an ontogenetic series of dolphins. The neutral zone is defined as the deformation exhibited with no measurable applied load. (B) The relative neutral zone (neutral zone/total length) for the same specimens. Vertical dotted lines distinguish different life-history stages.

 

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© The Company of Biologists Ltd 2008