The invention belongs to the technical field of wind tunnel tests, and particularly relates to a
precession simulation device for a spiral
flutter wind tunnel test. According to the invention, the design problem of the rotor craft spiral
flutter wind tunnel test device is solved, and the key influence parameters and influence rules of the spiral
flutter of the aircraft are researched by designing the
precession motion simulation device of the rotor craft. Rotation of the rotor wings can be realized in the wind tunnel, and the rotating speed of the rotor wings is adjusted through the motor. Meanwhile, pitching and deflection
modal decoupling of the rotating shaft of the rotating
system is achieved, and pitching and deflection
modal frequencies are independently adjustable; meanwhile, the axis of the
pitch axis and the axis of the
yaw axis coincide, so that pitching and
yaw freedom degree
coupling precession motion can be achieved under the effect of
gyroscopic moment. Meanwhile,
nacelle rotating
mass rotational
inertia,
nacelle weight and
mass center position adjustment can be achieved; and finally, the rotating speed of the rotating
mass such as the rotor wing and the
propeller hub can be adjusted through a speed adjusting motor, matching of the rotating speed and the incoming flow speed is guaranteed, and the spiral flutter state is achieved.