The wound ballistics literature contains several misconceptions about the physical effects of penetrating projectiles in tissue and tissue simulants. These can adversely affect the proper management of gunshot injuries, particularly in view of the ongoing threat of terrorist and criminal acts using assault rifles against civilians. The understanding of the wounding effects by military rifle bullets can be founded on the concept of energy transfer to the wound as applied to high-energy missile trauma. A substantial component of high-energy transfer in assault rifle injuries is manifested by the dynamic phenomenon of temporary cavitation, which is extensively reviewed with respect to its impact on the wound production and the associated controversy surrounding its consequences in soft tissue wounds. Part of this controversy emanates from misinterpretation of experimental data regarding the magnitude of the temporary cavity induced by high-velocity projectiles and the different conceptions of the tissue response to cavitation. The interaction between the projectile and tissue can lead to tumbling and possibly to deformation and fragmentation of the bullet, all of which strongly influence the energy transfer characteristics affecting both the temporary cavitation and the size of the permanent wound channel. Awareness of these effects can enhance perception of clinical and radiological findings suggestive of the wounding mechanism by various projectiles. LEVEL OF EVIDENCE Review/therapeutic, level V.

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A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction of short and long-range trajectories of small bullets via atmospheric flight to final impact point. The mathematical model is based on the full equations of motion set up in the no-roll body reference frame and is integrated numerically from given initial conditions at the firing site. The projectile maneuvering motion depends on the most significant force and moment variations, in addition to gravity and Magnus effect. The computational flight analysis takes into consideration the Mach number and total angle of attack effects by means of the variable aerodynamic coefficients. For the purposes of the present work, linear interpolation has been applied for aerodynamic coefficients from the official tabulated database. The developed computational method gives satisfactory agreement with published data of verified experiments and computational codes on atmospheric projectile trajectory analysis for various initial firing flight conditions. ___________________________________________________________________________________________ AbstractA full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction of short and long-range trajectories of small bullets via atmospheric flight to final impact point. The mathematical model is based on the full equations of motion set up in the no-roll body reference frame and is integrated numerically from given initial conditions at the firing site. The projectile maneuvering motion depends on the most significant force and moment variations, in addition to gravity and Magnus effect. The computational flight analysis takes into consideration the Mach number and total angle of attack effects by means of the variable aerodynamic coefficients. For the purposes of the present work, linear interpolation has been applied for aerodynamic coefficients from the official tabulated database. The developed computational method gives satisfactory agreement with published data of verified experiments and computational codes on atmospheric projectile trajectory analysis for various initial firing flight conditions. ___________________________________________________________________________________________ AbstractA full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction of short and long-range trajectories of small bullets via atmospheric flight to final impact point. The mathematical model is based on the full equations of motion set up in the no-roll body reference frame and is integrated numerically from given initial conditions at the firing site. The projectile maneuvering motion depends on the most significant force and moment variations, in addition to gravity and Magnus effect. The computational flight analysis takes into consideration the Mach number and total angle of attack effects by means of the variable aerodynamic coefficients. For the purposes of the present work, linear interpolation has been a...

Homemade guns may inflict serious injuries mainly depending on the shooting distance. A case of a male victim discovered dead with a head wound thought to be inflicted by a homemade gun firing modified ammunition is presented. Upon completion of the postmortem examination, the question of whether the homemade gun recovered on site was able to inflict such a wound arose. An experimental approach was employed to evaluate the ballistic characteristics and wounding pattern of the homemade gun and then compare it with the actual case. Ballistic gelatin with an incorporated bone simulant was used to model and approximate the behavior of the projectile when striking and penetrating the victim's head. The retention of the bullets' path in gelatin was verified through experimental shootings using the same homemade gun and similar type of projectiles. Analysis of the experimental shootings allowed for improved observation and documentation of the wounding pattern, thus confirming the initial hypothesis that the recovered homemade gun did in fact inflict the wound observed during the autopsy of the victim.