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介绍了尾翼稳定脱壳穿甲弹（ＡＰＦＳＤＳ）在Ｍ＝４．５时，弹托与弹身分离过程中的超音速流场气动特性，给出了沿弹托、弹身母线上的压力分布，分析了弹托对弹身的机械干扰和气动干扰
The aerodynamic characteristics of the supersonic flow field during the separation of the bouncer from the body of the tail stabilizer APFDSDS at M = 4.5 are introduced. The pressure distributions along the bouncer and the elastic body busbar are given. Bounce on the body of the mechanical interference and pneumatic interference