2019
DOI: 10.1007/s11630-019-1180-y
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Numerical Investigation of Circumferential Groove Casing Treatment in a Highly-Loaded Low-Reaction Transonic Compressor Rotor

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Cited by 8 publications
(1 citation statement)
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“…Müller et al 7 found in a study on transonic compressor rotor that the circumferential multi-groove near the leading edge delayed the occurrence of leading edge overflow by reducing the tip load to push the main flow/tip leakage flow interface downstream. A similar conclusion was reached in the research by Ross et al 8 and Zhu et al 9 . In addition to the location, the depth and width of groove also had an impact on the stability expansion capacity.…”
Section: Introductionsupporting
confidence: 86%
“…Müller et al 7 found in a study on transonic compressor rotor that the circumferential multi-groove near the leading edge delayed the occurrence of leading edge overflow by reducing the tip load to push the main flow/tip leakage flow interface downstream. A similar conclusion was reached in the research by Ross et al 8 and Zhu et al 9 . In addition to the location, the depth and width of groove also had an impact on the stability expansion capacity.…”
Section: Introductionsupporting
confidence: 86%