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Information propagation in a subsonic compressor

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Old   May 1, 2019, 15:34
Default Information propagation in a subsonic compressor
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Could someone please explain about the information propagating in a subsonic compressor?

As seen in the image, I have put numerical probes in the IGV, Rotor, Stator and casing treatment.

My question is that since information in a subsonic flow regime propagates in upstream direction, should the passing frequencies of the rotor, the stator and the casing treatment or their harmonics appear in the probe I placed in the IGV?

How about the casing treatment?
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Old   May 1, 2019, 18:56
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I would imagine so. But whether those frequencies are strong and significant enough to be seen between all the other noise is another matter.
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Old   May 2, 2019, 01:57
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How about the casing treatment?

Can the the passing frequency of IGV appear in the probe I placed in the casing treatment?

Does it mean that every component in a subsonic compressor feel the presence of other components regardless of their positions?
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Old   May 2, 2019, 02:41
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Theoretically, yes. But again, whether the signal from far away features is swamped by noise from other closer features is another matter.
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Old   May 17, 2019, 11:19
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Which one of instanteous or averaged data should be used to capture blade passing frequency?

I have used a probe which recordrs absoulte pressure.

When I analyse the FFT of this probe, I get half or less than the half of the blade passing frequency.

Why does this happen?
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