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An experimental investigation on the interaction between inlet swirl distortion and a low-speed axial compressor.

Sci Prog · 2020 · PMC10451049 · PMID 32672092

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an increasing trendno p-value reported
13 found that with the compressor throttled to the stall boundary, casing static pressure irregularity presents an increasing trend, and once a certain threshold was reached, the compressor was stalled.

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