振幅对流线型箱梁自激气动力的影响

Influence of vibration amplitude on motion-induced aerodynamic force of a streamline box girder

  • 摘要: 研究了强迫振动振幅对流线型箱梁断面自激气动力的影响。采用1:70的刚性节段模型开展了测压试验,获得了不同迎角的模型断面在不同振幅下的气动压力和分布,探讨了气动力特性。试验中的扭转振幅范围为2°~16°,竖向振幅范围为5~23mm,来流迎角分别为0°和±5°。测试结果表明,在迎角α=0°条件下,当扭转振幅At ≤8°,或竖向约化振幅Av/D≤0.46时,自激气动力的线性谐波占整体气动力的比例在95%以上,没有明显的高次谐波分量。当扭转振幅At > 8°,来流迎角为+5°时,自激气动力的线性谐波比例可降低到75%,高次谐波的比例可达到25%。扭转振幅对颤振导数A2*A3*H2*均存在显著的影响,但竖向振幅仅对H4*存在一定的影响。由此得出,尽管颤振导数随振幅的改变是非线性的,但在一定条件下(如8°扭转角以内),气动力本身不含有明显的高次谐波分量。

     

    Abstract: The influence of the vibration amplitude on the motion-induced aerodynamic force of the streamline box girder has been studied. Based on a 1:70 rigid sectional model and electronic pressure scanner valves, the aerodynamic force of the model has been obtained by wind tunnel tests. The range of the torsional amplitude is from 2° to 16°, the range of the vertical amplitude is from 5mm to 23mm, and the angles of attack are 0° and ±5°. At 0° angle of attack, when the torsional amplitude is less than 8° and the vertical reduced amplitude is less than 0.46, the proportions of the linear motion-induced aerodynamic force remain stable and are more than 95%. When the amplitude of the torsional vibration is greater than 8° and the angle of attack is +5°, the linear harmonic components decrease and the high-order harmonic ones increase with the increase of the amplitude. The change of flutter derivatives shows that the torsional amplitude affects A2*, A3* and H2* dramatically, which implies the nonlinear change of the aerodynamic force. However, the vertical amplitude only affects H4*, which is not the control parameter of flutter analysis, and has no influence on the other flutter derivatives. The brief conclusion is that although the force-amplitude behavior of a streamline box girder is nonlinear, there is no obvious high-order component in the motion-induced aerodynamic force under a certain amplitude, especially under 8° torsional amplitude.

     

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