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Response of shock train to high-frequency fluctuating backpressure in an isolator

机译:冲击波对隔离器中高频波动背压的响应

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摘要

Schlieren images and unsteady pressure measurements were collected to explore the response of a shock train to a high-frequency fluctuating backpressure in an isolator. High-frequency excitations (between 105 and 225 Hz) were applied in the downstream of an isolator, thus leading a forced shock train oscillation. The experimental results show that the fundamental frequency of a shock train oscillation is very close to the excitations, and the shock train motions can be judged by pressure measurements. The whole isolator can be divided into three parts, including the undisturbed zone, the shock train oscillation zone, and the backpressure-affected zone. Different cases of forcing frequencies were studied, and it is found that the amplitude of the shock train oscillation increases with the decreasing excitation frequency. Moreover, the most upstream position of shock train motions is not located at the place where the maximum standard deviation occurs under fluctuating backpressure condition. Thus, the maximum standard deviation method can no longer be used for shock train leading edge detection. Actually, the most upstream position of the shock train leading edge is located at the place where the excited frequency content disappears or the place where the oscillation amplitude decreases to near zero.
机译:收集了Schlieren图像和非稳态压力测量值,以探索冲击波对隔离器中高频波动背压的响应。在隔离器的下游施加了高频激励(介于105和225 Hz之间),从而导致了强制冲击波振荡。实验结果表明,冲击波振荡的基本频率非常接近激励,并且可以通过压力测量来判断冲击波的运动。整个隔离器可分为三个部分,包括不受干扰的区域,冲击波振荡区域和反压影响区域。研究了强迫频率的不同情况,发现随着激励频率的降低,冲击波列振荡的振幅增大。此外,在波动的背压条件下,冲击波运动的最上游位置不在最大标准偏差发生的位置。因此,最大标准偏差方法不能再用于冲击波前缘检测。实际上,冲击波前缘的最上游位置位于励磁频率成分消失的位置或振荡振幅减小至接近零的位置。

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  • 来源
    《Journal of propulsion and power》 |2017年第6期|1520-1528|共9页
  • 作者单位

    National University of Defense Technology, Changsha, China,Science and Technology on Scramjet Laboratory, China;

    National University of Defense Technology, Changsha, China,Science and Technology on Scramjet Laboratory, China;

    National University of Defense Technology, Changsha, China,Science and Technology on Scramjet Laboratory, China;

    National University of Defense Technology, Changsha, China,Science and Technology on Scramjet Laboratory, China;

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