“…During a self-turning OTS launch, with a gradually increasing attack angle, the missile experiences wide and extra-wide attack angles, and the aerodynamic characteristics of its external flow field become a complex unsteady problem (Li et al 2017). Teng (2018), Hechmi and Taieb (2012), Barnette et al (2012), Liu (2018), and Howison and Ekici (2013) explored this problem using wind tunnel tests and numerical simulations. Their results show the eddy current and hysteresis effects in the flow fields of axisymmetric slender bodies at subsonic and transonic high angles of attack.…”