The geometry of high angle of attack maneuvers and the implications for G _y -induced neck injuries

Introduction: Modern super agile fighter aircraft have significantly expanded maneuverability envelopes, often involving very high angles of attack (AOA) in the post-stall region. One such maneuver is the high AOA velocity vector roll. The geometry of this flight maneuver is such that during the roll there is a significant lateral G load imposed on the unrestrained head-neck complex of the pilot. Methods: A mathematical analysis of the geometric relationship determining the magnitude of ± G _y acceleration during high AOA maneuvering was conducted. This preliminary mathematical model is able to predict the G _y load imposed on the head-neck complex of the pilot for a given set of flight maneuver parameters. Results: The analysis predicts that at an AOA of 70 ^o and with a roll rate of 100 ^o · s ^-1, the lateral G developed will be approximately 3.5 G _y. Increasing the roll rate increases the lateral G component: at 200 ^o · s ^-1 the G _yload is more than ± G _y. Conclusions: There are serious potential implications of super agile maneuvers on the neck of the pilot. The G environment experienced by the pilot of super agile aircraft is increasingly multiaxial, involving ± G _x, ± G _y, and ± G _z. The level of lateral G developed during these dynamic flight maneuvers should not be underestimated, as such G loads can potentially lead to neck injuries. While aircraft become ever more capable, a full understanding of the biodynamic effects on the pilot while exploiting the agility of the aircraft still needs to be developed.