| Literature DB >> 26448781 |
Aditya Belwadi1, King H Yang2.
Abstract
Aortic injury (AI) leading to disruption of the aorta is an uncommon but highly lethal consequence of trauma in modern society. Most recent estimates range from 7,500 to 8,000 cases per year from a variety of causes. It is observed that more than 80% of occupants who suffer an aortic injury die at the scene due to exsanguination into the chest cavity. It is evident that effective means of substantially improving the outcome of motor vehicle crash-induced AIs is by preventing the injury in the first place. In the current study, 16 design of computer experiments (DOCE) were carried out with varying levels of principal direction of force (PDOF), impact velocity, impact height, and impact position of the bullet vehicle combined with occupant seating positions in the case vehicle to determine the effects of these factors on aortic injury. Further, a combination of real world crash data reported in the Crash Injury Research and Engineering Network (CIREN) database, Finite Element (FE) vehicle models, and the Wayne State Human Body Model-II (WSHBM-II) indicates that occupant seating position, impact height, and PDOF, in that order play, a primary role in aortic injury.Entities:
Mesh:
Year: 2015 PMID: 26448781 PMCID: PMC4568358 DOI: 10.1155/2015/269386
Source DB: PubMed Journal: Comput Math Methods Med ISSN: 1748-670X Impact factor: 2.238
Range of values for the five design factors chosen for the DOCE study.
| Number | Design factor | Range | |||
|---|---|---|---|---|---|
| Striking vehicle | |||||
| 1 | Bumper profile | Low | High | — | — |
| 2 | Impact position (mm) | −300 | 0 | +300 | — |
| 3 | PDOF (degrees) | 250 | 270 | 290 | 310 |
| 4 | Initial velocity (km/h) | 30 | 38.3 | 46.6 | 54.9 |
| 5 | Occupant position (mm) | −125 | 0 | +125 | — |
Note. Impact position and occupant position are determined from the center of the case vehicles' B-pillar.
Figure 1(a) Position of the impact vehicle, height of impact, and occupant seating position for Phase B simulations; (b) PDOF for Phase B simulations.
Latin square sampling for DOCE and output response variables; average maximum principal strain (AMPS) and maximum pressure in the aorta.
| Run # | Bumper profile height | Impact position (mm) | PDOF (degrees) | Velocity (km/h) | Occupant position (mm) | Maximum simulation time (ms) | AMPS | Time at AMPS (ms) | Maximum pressure (kPa) | Time at maximum pressure (ms) |
|---|---|---|---|---|---|---|---|---|---|---|
| 1 | Low | −300 | 290 | 30 | +125 | 56 | 0.1180 | 55 | 105.8 | 50 |
| 2 | Low | −300 | 270 | 38.3 | 0 | 65 | 0.2240 | 44 | 113.5 | 46 |
| 3 | High | −300 | 250 | 46.6 | −125 | 54 | 0.1650 | 54 | 148.0 | 48 |
| 4 | High | −300 | 310 | 54.9 | 0 | 33 | 0.0540 | 33 | 109.0 | 33 |
| 5 | Low | 0 | 270 | 54.9 | 0 | 52 | 0.3240 | 40 | 135.0 | 36 |
| 6 | Low | 0 | 290 | 46.6 | +125 | 46 | 0.1580 | 44 | 119.6 | 36 |
| 7 | High | 0 | 310 | 30 | 0 | 78 | 0.0675 | 78 | 104.4 | 70 |
| 8 | High | 0 | 250 | 38.3 | −125 | 64 | 0.1650 | 56 | 120.0 | 50 |
| 9 | Low | 0 | 310 | 46.6 | −125 | 80 | 0.2100 | 60 | 127.6 | 50 |
| 10 | Low | 0 | 250 | 54.9 | 0 | 44 | 0.2580 | 43 | 117.7 | 42 |
| 11 | High | 0 | 290 | 38.3 | 0 | 44 | 0.0330 | 43 | 104.3 | 42 |
| 12 | High | 0 | 270 | 30 | +125 | 70 | 0.1520 | 54 | 110.8 | 54 |
| 13 | Low | +300 | 250 | 38.3 | 0 | 72 | 0.2300 | 44 | 113.2 | 48 |
| 14 | Low | +300 | 310 | 30 | −125 | 80 | 0.0250 | 78 | 103.0 | 78 |
| 15 | High | +300 | 270 | 54.9 | +125 | 36 | 0.2350 | 34 | 149.0 | 34 |
| 16 | High | +300 | 290 | 46.6 | 0 | 76 | 0.1600 | 54 | 123.7 | 52 |
Average maximum principal strain (%) = lower surface average maximum tensile principal strain in the longitudinal axis of the aorta.
AMPS and maximum strain curves for each run are presented in Figure 5.
Figure 2AMPS: (a) main effects chart; (b) Pareto chart of combination effects.
Figure 3(a) Main effects chart: maximum pressure (kPa); (b) Pareto chart of combined effects.
Failure versus nonfailure values of AMPS and maximum pressure in the aorta assessed based on failure criterion.
| Failure runs | Nonfailure runs | Significance ( | |
|---|---|---|---|
| Failure criterion = 22.1% strain [ | |||
| Average AMPS | 0.247 ± 0.041 | 0.109 ± 0.058 | 0.001 |
| Maximum pressure (kPa) | 126.00 ± 14.15 | 114.86 ± 13.82 | 0.155 |
|
| |||
| Failure criterion = 120 kPa pressure [ | |||
| Average AMPS | 0.203 ± 0.061 | 0.129 ± 0.091 | 0.076 |
| Maximum pressure (kPa) | 131.85 ± 12.51 | 109.08 ± 5.017 | 0.003 |