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VELOCITY AND PRESSURE MEASUREMENTS OF A MACH 0.85 AXISYMMETRIC JET

机译:MACH 0.85轴对称射流的速度和压力测量

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The turbulent properties of a heated and unheated Mach 0.85 axisymmetric jet have been studied. The velocity field of the jet at static temperature ratios of 0.87 and 2.34, was measured in the streamwise radial plane using Particle Image Velocimetry. The velocity measurements were acquired between streamwise locations of 3D and 8D downstream from the nozzle exit.Proper Orthogonal Decomposition (POD) was applied to the velocity field using snapshot POD. The POD analysis showed that the eigenvalues of the heated jet had higher fraction of energy. The POD eigenfunctions or modes of the streamwise velocity of both jets were similar, while the POD modes of the radial velocity of both jets were very different. The POD modes of radial velocity of the unheated jet were symmetrical about the jet centerline, and the modes of the heated jet seemed to merge at the centerline. The near field pressure measurements were acquired just outside the shearlayer. A linear array of five pressure transducers was placed at 7°to the nozzle lipline, so that it would be parallel to the shear layer. The transducers in the array were spaced one diameter apart. Pressure measurements were acquired at stream-wise locations between 4.25D and 10.25D from the nozzle exit. Based on the slope of the pressure spectra. the propagating events in the two jets were identified. The POD was also applied to the pressure data, and the POD modes of the two jets were compared. The peak in the amplitude of the POD mode of the heated jet was at a higher frequency. With increasing mode numbers, the peak
机译:已经研究了加热和未加热的马赫数0.85轴对称射流的湍流特性。使用粒子图像测速法在流向径向平面中测量了静态温度比为0.87和2.34时射流的速度场。在喷嘴出口下游的3D和8D的流向位置之间获取速度测量值。使用快照POD将正确的正交分解(POD)应用于速度场。 POD分析表明,加热射流的特征值具有较高的能量分数。两股射流的POD本征函数或流向速度模式相似,而两股射流的径向速度的POD模式却非常不同。未加热射流的径向速度的POD模式关于射流中心线对称,并且加热射流的模式似乎在中心线合并。近场压力测量值是在剪切层外部获取的。将五个压力传感器的线性阵列与喷嘴唇线成7°放置,以使其平行于剪切层。阵列中的换能器间隔一个直径。从喷嘴出口在4.25D和10.25D之间的流向位置获取压力测量值。基于压力谱的斜率。确定了两架飞机的传播事件。 POD也被应用于压力数据,并且比较了两个喷嘴的POD模式。热射流的POD模式的振幅峰值处于较高频率。随着模式编号的增加,峰值

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