在高声强下测量了微圆孔处声激发射流的速度和微圆孔的非线性声阻抗。随声压级的增加声激发射流的速度增大，实验中射流速度在0-19m/s范围内变化，这表明出现一种强烈声整流现象；与此同时微圆孔声阻明显增大，而声抗减小，声抗最小值约是其线性值的0.7倍。此外实验结果还验证了一种微园孔声学非线性效应离散涡模型的合理性。
Both the velocity of the sound-excited jet flow at asmall circular orifice and the nonlinear impedance of the orifice are measured at high sound intensity. As the sound pressure level isincreased, the velocity of the sound-excited jet flow increases. Inthe present experiment the flow velocities in the orifice coverap proximately the range of 0 to 19 m/s, thereby showing that a type ofstrong acoustic streaming occurs. Consequently the orifice resistan cemarkedly increases with the increase of the SPL while theorifice reactance decreases to 0.7 of its linear value at itslowest point. Besides, the present experiment has verified one previou sdiscrete vortex model of the acoustic nonlinearity of a circular orifice.
参考文献
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