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1.
J Trauma ; 69(1): 179-84, 2010 Jul.
Artigo em Inglês | MEDLINE | ID: mdl-20173659

RESUMO

BACKGROUND: Primary blast injuries, specifically lung injuries, resulting from blast overpressure exposures are a major source of mortality for victims of blast events. However, existing pulmonary injury criteria are inappropriate for common exposure environments. This study uses Drosophila melanogaster larvae to develop a simple phenomenological model for human pulmonary injury from primary blast exposure. METHODS: Drosophila larvae were exposed to blast overpressures generated by a 5.1-cm internal diameter shock tube and their mortality was observed after the exposure. To establish mortality thresholds, a survival analysis was conducted using survival data and peak incident pressures. In addition, a histologic analysis was performed on the larvae to establish the mechanisms of blast injury. RESULTS: The results of the survival analysis suggest that blast overpressure for 50% Drosophila survival is greater than human threshold lung injury and is similar to human 50% survival levels, in the range of overpressure durations tested (1-5 ms). A "parallel" analysis of the Bass et al. 50% human survival curves indicates that 50% Drosophila survival is equivalent to a human injury resulting in a 69% chance of survival. Histologic analysis of the blast-exposed larvae failed to demonstrate damage to the dorsal trunk of the tracheal system; however, the presence of flocculent material in the larvae body cavities and tracheas suggests tissue damage. CONCLUSIONS: This study shows that D. melanogaster survival can be correlated with large animal injury models to approximate a human blast lung injury tolerance. Within the range of durations tested, Drosophila larvae may be used as a simple model for blast injury.


Assuntos
Lesão Pulmonar Aguda/patologia , Traumatismos por Explosões/patologia , Modelos Animais de Doenças , Drosophila melanogaster , Animais , Drosophila melanogaster/anatomia & histologia , Ondas de Choque de Alta Energia , Humanos , Larva/anatomia & histologia , Pulmão/patologia
2.
Aviat Space Environ Med ; 81(5): 453-9, 2010 May.
Artigo em Inglês | MEDLINE | ID: mdl-20464811

RESUMO

INTRODUCTION: Military aviators are susceptible to spinal injuries during high-speed ejection scenarios. These injuries commonly arise as a result of strains induced by extreme flexion or compression of the spinal column. This study characterizes the vertebral motion of two postmortem human surrogates (PMHS) during a simulated catapult phase of ejection on a horizontal decelerator sled. METHODS: During testing, the PMHS were restrained supinely to a mock ejection seat and subjected to a horizontal deceleration profile directed along the local z-axis. Two midsized males (175.3 cm, 77.1 kg; 185.4 cm, 72.6 kg) were tested. High-rate motion capture equipment was used to measure the three-dimensional displacement of the head, vertebrae, and pelvis during the ejection event. RESULTS: The two PMHS showed generally similar kinematic motion. Head injury criterion (HIC) results were well below injury threshold levels for both specimens. The specimens both showed compression of the spine, with a reduction in length of 23.9 mm and 45.7 mm. Post-test autopsies revealed fractures in the C5, T1, and L1 vertebrae. DISCUSSION: This paper provides an analysis of spinal motion during an aircraft ejection.The injuries observed in the test subjects were consistent with those seen in epidemiological studies. Future studies should examine the effects of gender, muscle tensing, out-of-position (of head from neutral position) occupants, and external forces (e.g., windblast) on spinal kinematics during aircraft ejection.


Assuntos
Aceleração/efeitos adversos , Aeronaves , Militares , Traumatismos da Coluna Vertebral/prevenção & controle , Coluna Vertebral/fisiopatologia , Medicina Aeroespacial , Fenômenos Biomecânicos , Cadáver , Simulação por Computador , Humanos , Masculino , Pessoa de Meia-Idade , Traumatismos da Coluna Vertebral/etiologia , Traumatismos da Coluna Vertebral/fisiopatologia , Estados Unidos
3.
J Biomech ; 42(11): 1656-63, 2009 Aug 07.
Artigo em Inglês | MEDLINE | ID: mdl-19497574

RESUMO

An accurate understanding of the relationship between pulmonary pressure and volume is required for modeling pulmonary mechanics in a variety of clinical applications. In this study the experimental techniques and mathematical formulations used to characterize viscoelastic materials are applied to characterize transient pulmonary compliance in juvenile swine. Fixed volumes of air were insufflated into 5 swine and held constant for 45 s while the transient decay in tracheal pressure was measured. An analytical model was developed using an optimization scheme that maximized the model fit to the experimental data over the entire time convolution. The initial injected volume was varied to assess the spatial and temporal linearity of the behavior. Model performance was assessed by comparing measured and predicted pressure during insufflations of erratic volume waveforms. It is concluded that the pulmonary impedance of healthy juveniles can be adequately described over a wide volume and frequency range using a relatively simple 5-parameter model that is linear both spatially and temporally.


Assuntos
Mecânica Respiratória , Sistema Respiratório , Animais , Fenômenos Biomecânicos , Criança , Humanos , Pulmão/fisiologia , Modelos Anatômicos , Modelos Animais , Modelos Teóricos , Pressão , Ventilação Pulmonar , Respiração Artificial/métodos , Suínos
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