12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference) 2006
DOI: 10.2514/6.2006-2579
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Sound Generation in Centrifugal Compressors

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Cited by 6 publications
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“…Furthermore, tonal noise and buzz-saw noise (noise peaks occur at shaft rotation frequency and its harmonics) become the main noise sources in supersonic flow conditions. 12 Meanwhile, broadband noise can be obtained within the entire frequency range of interest. Several narrow bands were detected at 1.5-3.5 kHz in compression-ignition engines and at 5-7 kHz in spark-ignition engines.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, tonal noise and buzz-saw noise (noise peaks occur at shaft rotation frequency and its harmonics) become the main noise sources in supersonic flow conditions. 12 Meanwhile, broadband noise can be obtained within the entire frequency range of interest. Several narrow bands were detected at 1.5-3.5 kHz in compression-ignition engines and at 5-7 kHz in spark-ignition engines.…”
Section: Introductionmentioning
confidence: 99%