The invention provides an aeroelastic model vibration test device with variable bending and torsional
modal stiffness, which comprises a plane moving mechanism, a
magneto-rheological damping device and a torsional stiffness device, and is characterized in that the
magneto-rheological damping device is mounted on the plane moving mechanism, and a model is connected with the
magneto-rheological damping device through the torsional stiffness device; the
torsional rigidity device comprises a connecting piece, a rotary shifting piece and an elastic mechanism, the connecting piece is connected to the magnetorheological damping device, the elastic mechanism is connected to the connecting piece, the rotary shifting piece is connected with the model, the rotary shifting piece and the magnetorheological damping device are coaxial, and the elastic mechanism is shifted to twist when the rotary shifting piece rotates. The
magnetorheological fluid is used for damping, the response is fast, the damping force is stable, and the
controllability is good; and through the plane moving mechanism and the
torsional rigidity device, the
coupling effect in the downwind direction, the transverse
wind direction and the torsional direction can be achieved, the test requirement of multi-degree-of-freedom structure response is met, and the complex dynamic characteristics of an actual structure under the wind load effect are reflected more truly.