The model can be used for aeroelasticstability analysis of the new tilt-rotor aircraft in high-speed forward flight.
所建模型为进行新型倾转旋翼机大速度飞行时气弹稳定性分析奠定了基础。
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The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelasticstability.
It is also seen that the transverse shear deformation and warping have effects on the aeroelasticstability of the rotor blade. These effects become larger at the higher thrust level.