| Literature DB >> 25923776 |
Zhijie Jack Tseng1, John J Flynn2.
Abstract
Performance of the masticatory system directly influences feeding and survival, so adaptive hypotheses often are proposed to explain craniodental evolution via functional morphology changes. However, the prevalence of "many-to-one" association of cranial forms and functions in vertebrates suggests a complex interplay of ecological and evolutionary histories, resulting in redundant morphology-diet linkages. Here we examine the link between cranial biomechanical properties for taxa with different dietary preferences in crown clade Carnivora, the most diverse clade of carnivorous mammals. We test whether hypercarnivores and generalists can be distinguished based on cranial mechanical simulation models, and how such diet-biomechanics linkages relate to morphology. Comparative finite element and geometric morphometrics analyses document that predicted bite force is positively allometric relative to skull strain energy; this is achieved in part by increased stiffness in larger skull models and shape changes that resist deformation and displacement. Size-standardized strain energy levels do not reflect feeding preferences; instead, caniform models have higher strain energy than feliform models. This caniform-feliform split is reinforced by a sensitivity analysis using published models for six additional taxa. Nevertheless, combined bite force-strain energy curves distinguish hypercarnivorous versus generalist feeders. These findings indicate that the link between cranial biomechanical properties and carnivoran feeding preference can be clearly defined and characterized, despite phylogenetic and allometric effects. Application of this diet-biomechanics linkage model to an analysis of an extinct stem carnivoramorphan and an outgroup creodont species provides biomechanical evidence for the evolution of taxa into distinct hypercarnivorous and generalist feeding styles prior to the appearance of crown carnivoran clades with similar feeding preferences.Entities:
Mesh:
Year: 2015 PMID: 25923776 PMCID: PMC4414467 DOI: 10.1371/journal.pone.0124020
Source DB: PubMed Journal: PLoS One ISSN: 1932-6203 Impact factor: 3.240
Fig 1Species, relationships, and anatomical landmarks used for FE and GMM analyses.
A. Phylogenetic relationships for the species sample [56], with names of more inclusive clades indicated at internal nodes. The outgroup species is the creodont Thinocyon velox; creodonts are close relatives of Carnivoramorpha, together forming the Ferae [50]. B. Dorsal view of anatomical fixed and semi-landmarks. C. Ventral view of landmarks. D. Dorso-lateral view of landmarks on a generic skull representing the average shape of species examined.
Anatomical landmarks and surface semi-landmarks used in GMM analyses.
| No. | Description |
|---|---|
| 1 | Mid-sagittal premaxillary suture at dorsal base of I1 crown |
| 2 | Mid-sagittal nasal suture, anterior-most edge |
| 3 | Mid-sagittal position of anterior rim of orbit from dorsal view |
| 4 | Mid-sagittal position of postorbital constriction |
| 5 | Posterior point of sagittal crest |
| 6 | Midsagittal ventral border of foramen magnum |
| 7 | Posterior mid-sagittal border of palate |
| 8 | Mid-sagittal premaxillary suture at ventral base of I1 crown |
| 9 | Inflection point of the narial ridge of the premaxilla from lateral view (right side) |
| 10 | Anterior border between the maxilla and canine (right side) |
| 11 | Rostral border of the first tooth in the cheek dentition at the ventral surface of the maxilla (right) |
| 12 | Rostro-dorsal border of the infraorbital foramen (right side) |
| 13 | Ventral-most point of the orbital rim edge (right side) |
| 14 | Tip of the postorbital process of the frontal (right side) |
| 15 | Tip of the postorbital process of the jugal (right side) |
| 16 | Base of the zygomatic arch at the caudal-facing face of the maxilla (right side) |
| 17 | Inflection point of the palate and the pterygoid process (right side) |
| 18 | Inflection point of the pterygoid process and the ventral-facing basicranial plane (right side) |
| 19 | Rostral border of the medial origin of the zygomatic arch on the squamosal (right side) |
| 20 | Lateral-most point of the zygomatic arch, at its dorsoventrally centered point (right side) |
| 21 | Medial base of the glenoid ridge/process (right side) |
| 22 | Caudal border of the medial origin of the zygomatic arch on the squamosal (right side) |
| 23 | Rostral base of the occipital condyle (right side) |
| 24 | Inflection point of the narial ridge of the premaxilla from lateral view (left side) |
| 25 | Anterior border between the maxilla and canine (left side) |
| 26 | Rostral border of the first tooth in the cheek dentition at the ventral surface of the maxilla (left) |
| 27 | Rostro-dorsal border of the infraorbital foramen (left side) |
| 28 | Ventral-most point of the orbital rim edge (left side) |
| 29 | Tip of the postorbital process of the frontal (left side) |
| 30 | Tip of the postorbital process of the jugal (left side) |
| 31 | Base of the zygomatic arch at the caudal-facing face of the maxilla (left side) |
| 32 | Inflection point of the palate and the pterygoid process (left side) |
| 33 | Inflection point of the pterygoid process and the ventral-facing basicranial plane (left side) |
| 34 | Rostral border of the medial origin of the zygomatic arch on the squamosal (left side) |
| 35 | Lateral-most point of the zygomatic arch, at its dorsoventrally centered point (left side) |
| 36 | Medial base of the glenoid ridge/process (left side) |
| 37 | Caudal border of the medial origin of the zygomatic arch on the squamosal (left side) |
| 38 | Rostral base of the occipital condyle (left side) |
| 39–59 | Left temporalis muscle attachment region, anchored by landmarks 4, 5, 34, 36, 37 |
| 60–80 | Right temporalis muscle attachment region, anchored by landmarks 4, 5, 19, 21, 22 |
| 81–103 | Left masseter muscle attachment region, anchored by landmarks 30, 35 |
| 104–126 | Right masseter muscle attachment region, anchored by landmarks 15, 20 |
Landmarks 1–38 are fixed landmarks, 39–126 are surfaces with semi-landmarks.
Fig 2Regression analyses of FE analyses on upper dentitions.
Results bracketing the entire dentition are shown by species values at the first tooth position (dark circles) and the last tooth position (hollow circle) for parts A, C, and D.A. Output bite force versus input load, in Newtons. B. Input load versus total model volume, circles represent species values, with the outlier Panthera pardus indicated by a hollow circle. The two upper fitted curves represent exponential and linear regressions without the outlier. The bottom curve shows regression incorporating the outlier. C. Total strain energy versus total model volume. Both regressions did not include the outlier. D. Strain energy versus input load. Regression analyses were conducted with and without Panthera pardus because that species has outlying values for both input load and strain energy estimates. The last tooth position (hollow circles) may be a different locus in taxa sampled, ranging from M1 to M3, because of evolutionary loss of teeth at the posterior end of the tooth row. Abbreviations: Cl, Canis lupus; Hj, Herpestes javanicus; Mm, Mephitis mephitis; Oh, Oodectes herpestoides; Pl, Procyon lotor; Pp, Panthera pardus; Tv, Thinocyon velox.
Summary of FEA (n = 264 analyses).
| MODEL | Lores | Medres | Hires | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| SIDE | Left | Right | Left | Right | Left | Right | |||||||
| ATTRIBUTE | BF | SE | BF | SE | BF | SE | BF | SE | BF | SE | BF | SE | |
|
| C | 242 | 0.092 | 267 | 0.096 | 251.5 | 0.115 | 248.2 | 0.109 | 241.1 | 0.115 | 248.4 | 0.115 |
| P1 | 287 | 0.094 | 288 | 0.089 | 274.2 | 0.109 | 268.3 | 0.104 | 268.9 | 0.109 | 263.5 | 0.107 | |
| P2 | 334 | 0.099 | 331 | 0.089 | 316.9 | 0.109 | 309.1 | 0.1 | 308.5 | 0.11 | 301.1 | 0.103 | |
| P3 | 369 | 0.089 | 384 | 0.086 | 362.1 | 0.1 | 373 | 0.098 | 349.6 | 0.102 | 349.4 | 0.1 | |
| P4 | 461 | 0.092 | 454 | 0.083 | 436.1 | 0.1 | 423.9 | 0.093 | 423.3 | 0.1 | 415 | 0.096 | |
| M1 | 556 | 0.094 | 562 | 0.076 | 530.9 | 0.094 | 522.9 | 0.086 | 512 | 0.089 | 511.7 | 0.087 | |
|
| M2 | 463 | 0.087 | 685 | 0.099 | 650.3 | 0.084 | 645.5 | 0.121 | 625.4 | 0.081 | 628.7 | 0.084 |
|
| C | 30.4 | 0.002 | 30.9 | 0.002 | 28.22 | 0.003 | 28.23 | 0.003 | 29.65 | 0.002 | 29.67 | 0.003 |
| P1 | 34 | 0.002 | 34.7 | 0.002 | 31.54 | 0.002 | 31.79 | 0.003 | 33.19 | 0.002 | 33.39 | 0.002 | |
| P2 | 37.5 | 0.002 | 38.2 | 0.002 | 34.65 | 0.003 | 34.59 | 0.003 | 36.6 | 0.003 | 36.44 | 0.002 | |
| P3 | 43.2 | 0.002 | 43.2 | 0.002 | 39.38 | 0.003 | 39.49 | 0.003 | 41.3 | 0.002 | 41.41 | 0.002 | |
| P4 | 48.7 | 0.002 | 49.6 | 0.002 | 45.36 | 0.002 | 45.34 | 0.002 | 46.92 | 0.002 | 47.11 | 0.002 | |
| M1 | 18.5 | 0.002 | 58 | 0.002 | 52.94 | 0.002 | 53.03 | 0.002 | 55.44 | 0.002 | 55.45 | 0.002 | |
|
| M2 | 66.5 | 0.002 | 67.4 | 0.002 | 60.22 | 0.002 | 60.6 | 0.002 | 63.36 | 0.002 | 63.36 | 0.002 |
|
| C | 22.7 | 0.002 | 21.4 | 0.002 | 23.45 | 0.002 | 22.87 | 0.002 | 20.48 | 0.003 | 20.48 | 0.003 |
| P2 | 27.8 | 0.002 | 24 | 0.002 | 26.37 | 0.002 | 25.42 | 0.002 | 22.8 | 0.003 | 22.8 | 0.003 | |
| P3 | 28.8 | 0.002 | 25.1 | 0.002 | 28.31 | 0.002 | 26.85 | 0.002 | 24.25 | 0.003 | 23.91 | 0.003 | |
| P4 | 30.7 | 0.002 | 29.4 | 0.002 | 32.08 | 0.002 | 30.94 | 0.002 | 27.15 | 0.003 | 28.18 | 0.003 | |
|
| M1 | 36.1 | 0.002 | 33.9 | 0.002 | 37.21 | 0.002 | 36.53 | 0.002 | 31.76 | 0.003 | 32.2 | 0.003 |
|
| C | 35.5 | 0.004 | 35.5 | 0.004 | 36.73 | 0.005 | 35.97 | 0.005 | 39.72 | 0.005 | 39.47 | 0.004 |
| P2 | 42.9 | 0.004 | 43.1 | 0.004 | 44.56 | 0.004 | 43.71 | 0.005 | 48.05 | 0.004 | 47.8 | 0.004 | |
| P3 | 48.3 | 0.004 | 48.3 | 0.004 | 49.64 | 0.004 | 48.75 | 0.005 | 54.31 | 0.004 | 53.88 | 0.004 | |
| P4 | 53.8 | 0.004 | 53.9 | 0.004 | 56.23 | 0.004 | 55.21 | 0.005 | 60.02 | 0.004 | 60.54 | 0.004 | |
| M1 | 60.3 | 0.004 | 60.8 | 0.004 | 63.19 | 0.004 | 62.31 | 0.005 | 68.14 | 0.004 | 68.5 | 0.004 | |
| M2 | 67.4 | 0.003 | 68.6 | 0.004 | 71.49 | 0.004 | 70.75 | 0.005 | 76.29 | 0.004 | 76.62 | 0.004 | |
|
| M3 | 74.1 | 0.003 | 75.1 | 0.004 | 77.99 | 0.004 | 77.01 | 0.005 | 84.84 | 0.004 | 84.27 | 0.004 |
|
| C | 202 | 0.034 | 158 | 0.039 | 312.1 | 0.041 | 314.4 | 0.044 | 305.3 | 0.038 | 311.3 | 0.039 |
| P2 | 227 | 0.027 | 188 | 0.034 | 367 | 0.036 | 371.9 | 0.041 | 358.1 | 0.036 | 365.6 | 0.035 | |
| P3 | 283 | 0.027 | 208 | 0.036 | 415.9 | 0.039 | 426 | 0.037 | 406.3 | 0.035 | 418.6 | 0.042 | |
| P4 | 360 | 0.027 | 254 | 0.037 | 496 | 0.045 | 524.5 | 0.044 | 490.7 | 0.038 | 510 | 0.045 | |
|
| C | 74.5 | 0.011 | 74.6 | 0.012 | 85.84 | 0.013 | 88.02 | 0.014 | 83.3 | 0.014 | 84.19 | 0.015 |
| P1 | 52.9 | 0.01 | 81.4 | 0.012 | 94.26 | 0.013 | 97.22 | 0.014 | 89.57 | 0.014 | 90.08 | 0.014 | |
| P2 | 85.3 | 0.011 | 85.8 | 0.012 | 101.2 | 0.013 | 103.6 | 0.014 | 97.29 | 0.014 | 97.52 | 0.014 | |
| P3 | 59.6 | 0.01 | 96 | 0.012 | 109.8 | 0.013 | 111.6 | 0.013 | 106.7 | 0.014 | 108.4 | 0.014 | |
| P4 | 106 | 0.01 | 105 | 0.011 | 126.4 | 0.012 | 123.9 | 0.013 | 120.6 | 0.013 | 117.3 | 0.013 | |
| M1 | 140 | 0.009 | 121 | 0.01 | 144.1 | 0.012 | 145.9 | 0.012 | 139.3 | 0.012 | 137.4 | 0.012 | |
|
| M2 | 140 | 0.009 | 144 | 0.01 | 168.3 | 0.011 | 173.2 | 0.011 | 169.7 | 0.012 | 164.7 | 0.012 |
|
| C | 22.9 | 0.002 | 22.2 | 0.002 | 25.49 | 0.002 | 25.32 | 0.002 | 25.28 | 0.002 | 25.31 | 0.002 |
| P1 | 26.8 | 0.002 | 25.9 | 0.002 | 29.86 | 0.002 | 29.24 | 0.002 | 29.69 | 0.002 | 29.47 | 0.002 | |
| P2 | 30.6 | 0.002 | 29.8 | 0.002 | 34.22 | 0.002 | 32.88 | 0.002 | 33.78 | 0.002 | 33.31 | 0.002 | |
| P3 | 35.5 | 0.002 | 34.2 | 0.002 | 39.3 | 0.002 | 38.94 | 0.002 | 39.01 | 0.002 | 39.27 | 0.002 | |
| P4 | 39.8 | 0.002 | 38.4 | 0.002 | 44.45 | 0.002 | 44.77 | 0.002 | 44 | 0.002 | 44.57 | 0.002 | |
| M1 | 46.8 | 0.002 | 45.2 | 0.002 | 52.73 | 0.002 | 52.92 | 0.002 | 52.82 | 0.002 | 52.94 | 0.002 | |
|
| M2 | 56.1 | 0.002 | 54 | 0.002 | 62.84 | 0.002 | 62.59 | 0.002 | 62.24 | 0.002 | 62.94 | 0.002 |
BF: bite force (in Newtons), SE: strain energy (in Joules). Lores, Medres, and Hires models correspond roughly to 500k, 1,000k, and 1,500k tetrahedral elements, respectively. Canis lupus input force: 2509.99 N, volume: 207926 mm3, specimen LACM(M)23010. Herpestes javanicus input force: 262.21 N, volume: 10224 mm3, specimen AMNH(M)101655. Mephitis mephitis input force: 217.42 N, volume: 8856 mm3, specimen AMNH(M)172133. Oodectes herpestoides input force: 262.08 N, volume: 7947 mm3, specimen AMNH140008. Panthera pardus input force: 2168.94 N, volume: 40912 6mm3, specimen AMNH(M)113745. Procyon lotor input force: 650.91 N, Volume: 37352 mm3, specimen AMNH(M)24815. Thinocyon velox input force: 261.51 N, Volume: 11658 mm3, specimen FMNH PM60215. Seven bite positions were simulated for all species except for two species that have lower tooth counts: Mephitis mephitis (5 bite positions) and Panthera pardus (4 bite position). Institutional abbreviations: AMNH, American Museum of Natural History; FMNH, Field Museum of Natural History; LACM, Natural History Museum of Los Angeles County; M, Mammalogy collection.
Scaling relationships of FEA results.
| Position | Regression Equation | r2 | RMA slope | Isometry slope | Pearson Product-Moment Corr. Coef. |
| Scaling | |
|---|---|---|---|---|---|---|---|---|
| Input Load-Bite Force | Canine |
| 0.9817 | 1.02 | 1 | 0.9903 |
| Isometry |
| Last tooth |
| 0.9768 | 1.04 | 1 | 0.9842 |
| Isometry | |
| Volume-Input Load | all |
| 0.7787 | 0.51 | 0.66 | 0.6721 | 0.05 | - |
| w/o |
| 0.9981 | 0.49 | 0.66 | 0.458 | 0.18 | - | |
| Volume-Strain Energy | Canine |
| 0.3714 | 0.74 | 1 | 0.6177 | 0.07 | - |
| Last tooth |
| 0.4298 | 0.75 | 1 | 0.6491 | 0.06 | - | |
| w/o | Canine |
| 0.9972 | 0.79 | 1 | 0.4316 | 0.2 | - |
| Last tooth |
| 0.9965 | 0.78 | 1 | 0.4569 | 0.18 | - | |
| Input Load-Strain Energy | Canine |
| 0.9598 | 1.464 | 1.5 | 0.9806 |
| Negative allometry |
| Last tooth |
| 0.952 | 1.4807 | 1.5 | 0.9855 |
| Negative allometry | |
| w/o | Canine |
| 0.9708 | 1.6107 | 1.5 | 0.9832 |
| Positive allometry |
| Last tooth |
| 0.9676 | 1.5788 | 1.5 | 0.9824 |
| Positive allometry | |
| Bite Force-Strain Energy | Canine |
| 0.9528 | 1.4348 | 1.5 | 0.9838 |
| Negative allometry |
| Last tooth |
| 0.9545 | 1.4271 | 1.5 | 0.9844 |
| Negative allometry |
Regression analyses were conducted on both raw values and phylogenetic independent contrasts. Homologous canine positions and analogous most posterior tooth positions were tested.
*Statistically significant result at p = 0.001.
Fig 3Biting biomechanics profiles of all skull models.
A. Strain energy versusoutput bite force. B. Corrected strain energy versus mechanical efficiency, with strain energy values of each sampled species x, adjusted relative to C. lupus (“x adjusted”) using the equation: SE = (Volume/Volume)1/3(InputLoad/InputLoad)2*SE[28]. C. ME-SE profiles from part B categorized according to ecomorphs, with x and y axes representing relative magnitudes of mechanical efficiency and corrected strain energy, respectively. D. ME-SE profiles of the 5 extant species models constructed in this study (marked as caniform or feliform by line color only, no point labels), plus 6 additional species models taken from the literature (marked by circles for caniform and triangles for feliform species) [39,40,44,45]. Note general separation between caniform and feliform curves, the one exception being Lycaon pictus. Abbreviations as in Fig 2.
Fig 4von Mises stress distributions across bite positions in different species.
Visualized colors are standardized to 10% of max von Mises stress values in each bite analysis of every skull model to show the distribution of the most widespread stress locations. Elevated stress values are indicated by lighter blue color, whereas low or no-stress regions are in darer blue. Dotted boxes indicate bite positions in hypercarnivores that show optimal ME-SE ratios, as in Fig 3C.
Fig 5Phylomorphospace derived from GMM analyses and major directions of cranial shape change shown using morphed skulls of the average shape among species studied.
A. PC1-2 plot of fixed landmark analysis. B. PC1-2 plot of sliding semi-landmarks analysis with bending energy superimposition. C. PC1-2 plot of sliding semi-landmarks analysis with Procrustes superimposition. D. Directions of skull shape change along the first two PC axes in the fixed landmark analysis. E. Directions of skull shape change along the first two PC axes in the semi-landmarks analysis with bending energy superimposition. F. Directions of skull shape change along the first two PC axes in the semi-landmarks analysis with Procrustes superimposition.
Fig 6Cranial shape changes in morphed models, associated with A. input load / body size increase or decrease, and B. strain energy differences (higher or lower stiffness).
Skulls were morphed from the model of O. herpestoides using trends from regression analyses of phylogenetic independent contrasts of input load, strain energy, and geometric skull shape.