对３≤Ｍ∞≤１０马赫数范围的旋转稳定炮弹作了阻力与稳定性的理论分析。并给出了多种几何外形炮弹的压力、表面摩擦力、底部阻力及总阻力随马赫数的变化规律。提出了各种发射条件下相同炮弹结构的陀螺稳定性，动力学稳定性及其它稳定参数。给出的这些结果说明，为了同时获得低阻力和高超音速下的稳定飞行应该考虑的设计协调问题 The theoretical analysis of the resistance and stability of the stable rotating projectile with the range of 3≤M∞≤10 Mach was made. The laws of pressure, surface friction, bottom resistance and total resistance with Mach number for a variety of geometrical shells are given. The gyroscopic stability, dynamic stability and other stability parameters of the same shell structure under various launching conditions are proposed. These results are given to illustrate the design coordination issues that should be considered in order to achieve both low drag and stable flight at hypersonic speeds