Volume 7: Turbomachinery, Parts A, B, and C 2011
DOI: 10.1115/gt2011-45502
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A Method to Estimate the Performance Map of a Centrifugal Compressor Stage

Abstract: A novel approach to calculate the performance map of a centrifugal compressor stage is presented. At the design point four non-dimensional parameters (the flow coefficient φ, the work coefficient λ, the tip-speed Mach number M and the efficiency η) characterize the performance. In the new method the performance of the whole map is also based on these four parameters through physically-based algebraic equations which require little prior knowledge of the detailed geometry. The variable empirical coefficients in… Show more

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Cited by 11 publications
(17 citation statements)
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“…As stated by many authors, 21,25 limiting M 1 rel is necessary to design high-efficiency compressors. For this end, two variants are possible: the first one is to search the geometric parameters limiting the M 1 rel by a complex optimization under constraints, which is the standard method (minimization of M 1 rel ).…”
Section: Description Of the Proposed Inputs-generatormentioning
confidence: 99%
See 1 more Smart Citation
“…As stated by many authors, 21,25 limiting M 1 rel is necessary to design high-efficiency compressors. For this end, two variants are possible: the first one is to search the geometric parameters limiting the M 1 rel by a complex optimization under constraints, which is the standard method (minimization of M 1 rel ).…”
Section: Description Of the Proposed Inputs-generatormentioning
confidence: 99%
“…For a constant flow rate and rotational speed, when the inducer tip diameter is increased the axial velocity will be reduced, but the vane speed will be important leading to a large relative velocity. Consequently, these different investigations 21,23–25 have recommended some values or ranges for the different useful design parameters.…”
Section: Introductionmentioning
confidence: 99%
“…Determining turbocharger design is simplified using a initial design method for estimating compressor and turbine performance maps with only limited design parameter inputs. For compressor map estimation, the authors have selected to use the method of previous literature works 3638 where both optimum compressor design and resulting compressor map are estimated.…”
Section: System Descriptionmentioning
confidence: 99%
“…Together with the efficiency, the performance of the compressor is completely defined. 17 The relation between the dimensionless coefficients proposed by Jensen, defined in equation (4), is controlled with six adjustable parameters that are calibrated with a least squares method using all the available points in the measured compressor map…”
Section: Literature Backgroundmentioning
confidence: 99%