在高速流动中，边界层转捩不仅会显著增加热流，影响热防护设计，还会改变飞行器表面的气动力载荷，进而改变静/动稳定性，对飞行安全和操控特性带来影响，因此转捩是高性能气动设计关注的重要气动问题之一。以半锥角7°尖锥马赫数为6的流动为研究对象，在∅1 m常规高速风洞中开展了强迫振动动导数测量试验，同步测量了红外热图，不仅获得了不同雷诺数、攻角下俯仰力矩静/动导数，而且得到了清晰的转捩阵面，通过二者对比分析了静/动稳定性与转捩位置的关系，并通过典型转捩流动的定常数值模拟分析了气动力矩特性改变的机制，弥补了之前研究手段的不足，进一步明确了转捩与动态气动特性之间的关系和物理机制。研究结果表明：转捩对动态气动特性的影响与转捩区域相对质心的位置密切相关，当转捩阵面处于质心下游区域时，静/动稳定性会发生显著改变；转捩发生后引起壁面压力、摩阻的非对称变化是导致静/动稳定性改变的根本原因，其中摩阻在转捩引起的附加力矩中具有和压力相当的作用。

In high-speed flows， boundary layer transition will not only significantly increase heat-flux and affect the thermal protection design， but also change aerodynamic load on aircraft surface， and then change static/dynamic stability. This will have an impact on the flight safety and control characteristics of aircraft， so transition is one of the important aerodynamic issues in high-performance aerodynamic design. In the present study， the test of forced vibration dynamic derivative measurement is carried out in a ∅ 1 m conventional high-speed wind tunnel with a 7° half-angle sharp cone at Mach number 6， and the infrared thermogram is measured simultaneously. Not only the static/dynamic derivatives of pitching moment at different Reynolds numbers and angles of attack， but also a series of clear transition front are obtained. By comparing them， the relationship between static/dynamic stability and transition position is analyzed， and the mechanism of change of aerodynamic moment characteristics is analyzed by steady numerical simulation of typical transition flow. The study makes up for the deficiency of previous research methods， and further clarifies the relationship and physical mechanism between transition and dynamic aerodynamic characteristics. The results show that the influence of transition on dynamic aerodynamic characteristics is closely related to the position of the transition region relative to the center of mass， and the static/dynamic stability will change significantly when the transition front is in the downstream region of the center of mass. The asymmetric change of wall pressure and friction caused by transition is the fundamental reason for the change of static/dynamic stability， and friction plays an equal role as pressure in the additional moment induced by transition.