2022
DOI: 10.1115/1.4053707
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Efficient Optimization Design of Vortex Generators in a Highly Loaded Compressor Stator

Abstract: Secondary flow transfers the boundary layer from endwall to suction side corner region, which deteriorates the performance of compressors. Vortex Generators (VGs) can attenuate the secondary flow when implemented at the endwall of blade passage. In order to make an efficient optimization design of the VGs layout, mathematical models are introduced to replace the actual VGs. However, the model is only effective at small incidence less than 20 degrees. In this paper, firstly, a mathematical model is presented to… Show more

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Cited by 2 publications
(1 citation statement)
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“…With respect to the assessment of the overall aerodynamic loss of the axial flow blades, in many investigations [2][3][4], this loss can be conveniently evaluated by measuring the pressure parameters at the entrance and exit of the blade passage and calculating the Entropy 2023, 25, 1293 2 of 19 relative total pressure loss coefficient; however, the relative total pressure loss coefficient is a cumulative quantity, so this coefficient cannot express the local contribution to the loss very intuitively.…”
Section: Introductionmentioning
confidence: 99%
“…With respect to the assessment of the overall aerodynamic loss of the axial flow blades, in many investigations [2][3][4], this loss can be conveniently evaluated by measuring the pressure parameters at the entrance and exit of the blade passage and calculating the Entropy 2023, 25, 1293 2 of 19 relative total pressure loss coefficient; however, the relative total pressure loss coefficient is a cumulative quantity, so this coefficient cannot express the local contribution to the loss very intuitively.…”
Section: Introductionmentioning
confidence: 99%