This model is specially developed for Electrical Controlled Rotor aeroelastic analysis, and can take account of the unsteady effect of flap nose overhang.

• 为满足电控旋翼的气弹分析需要,给出了带襟翼翼型的综合时域非定常气动力模型,该模型可以计及襟翼移轴补偿的影响。