2017
DOI: 10.3390/ijtpp2040019
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Analysis of Vaneless Diffuser Stall Instability in a Centrifugal Compressor

Abstract: Abstract:Numerical simulations based on the large eddy simulation approach were conducted with the aim to explore vaneless diffuser rotating stall instability in a centrifugal compressor. The effect of the impeller blade passage was included as an inlet boundary condition with sufficiently low flow angle relative to the tangent to provoke the instability and cause circulation in the diffuser core flow. Flow quantities, velocity and pressure, were extracted to accumulate statistics for calculating mean velocity… Show more

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Cited by 13 publications
(4 citation statements)
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References 23 publications
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“…A bounded central differencing scheme is used as a convection scheme. This scheme has been utilized previously in past studies 37,38 utilizing the LES approach in STAR-CCM + .…”
Section: Methodsmentioning
confidence: 99%
“…A bounded central differencing scheme is used as a convection scheme. This scheme has been utilized previously in past studies 37,38 utilizing the LES approach in STAR-CCM + .…”
Section: Methodsmentioning
confidence: 99%
“…LES proved able to predict the frequencies associated with the early stage of stall, while the detailed flow visualizations were helpful in following the stall mechanism in view of an improved redesign. More recently, the problem of a vaneless diffuser stall was investigated by LES of a simplified diffuser-like geometry that included the cavities around the impeller trailing edge [136]. In that case, LES shed some light on the development of reverse flow in the radial diffuser when running the compressor close to the left operating limit, revealing the close link that exists between the periodic perturbations from the impeller and the diffuser instability.…”
Section: Centrifugal Compressorsmentioning
confidence: 99%
“…A well-designed diffuser decreases the flow instabilities coming from the impeller outlet, as well as energy losses. However, under off-design conditions, the flow field within the vaneless diffuser could be stalled due to boundary layer separation or core flow instability; the mechanisms and characteristics of this type of rotating stall have been extensively studied, theoretically [22][23][24][25], experimentally [26][27][28][29][30][31][32], and numerically [33][34][35][36][37][38][39]. The topology of rotating stall cells in the vaneless diffuser is shown in Figure 2, the characteristics of which can be briefly summarized as follows:…”
Section: Introductionmentioning
confidence: 99%