Abstract
Corner separation (CS) which can lead to deleterious consequences is an inherent flow structure in compressor. Two new suction slot configurations (SSCs) were proposed to investigate effects of boundary layer suction (BLS) on CS in a linear highly loaded compressor cascade. Five SSCs, under the same suction mass flows of 0.7 % of the inlet mass flows, were numerically studied over a range of operation incidence angles. The results were compared for different SSCs. Then the flow details were systematically analyzed to reveal the flow mechanisms.
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Liu, Y., Sun, J., & Lu, L. (2016). Control of corner separation in a linear highly loaded compressor cascade by boundary layer suction. In Lecture Notes in Mechanical Engineering (pp. 307–311). Springer Heidelberg. https://doi.org/10.1007/978-3-662-48868-3_49
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