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Experimental analysis of the near field pressure of a single stream subsonic jet

机译:单流亚音速射流近场压力的实验分析

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Measurements of the near field pressure around a single stream jet were performed in Cepra19, the anechoic wind tunnel of Onera, by means of an azimuthal array of microphones. Isothermal and heated jet were studied at the same 0.7 jet Mach number. Some tendencies observed in the experimental results are linked to the hydrodynamic and acoustic pressure fields present in the near field pressure. Numerical calculations and stability analysis will be performed in order to link these tendencies to non-linear behaviour.
机译:在单流射流附近的近场压力的测量是在Cepra19(Onera的无声风洞)中通过麦克风的方位角阵列进行的。在相同的0.7射流马赫数下研究了等温和加热射流。实验结果中观察到的一些趋势与近场压力中存在的流体动力和声压场有关。为了将这些趋势与非线性行为联系起来,将进行数值计算和稳定性分析。

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