2009
DOI: 10.1243/09576509jpe643
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A procedure for the design of radial cascade diffusers based on the maximum ratio between flow deflection and total pressure loss coefficient

Abstract: A design procedure of radial cascade diffusers for incompressible flow, based on the maximum ratio between the flow deflection and the total pressure loss coefficient, is proposed. To achieve such a result, numerical investigations were carried out on several different diffusers at design and off-design operating conditions. Four space chord ratios, with seven blades and nine outlet flow angles were considered. For each diffuser, the optimum performance parameters were correlated to the incoming flow angle and… Show more

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Cited by 1 publication
(2 citation statements)
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“…Pampreen 3 provided some results from experience with the use of a cascade in the design of diffuser for the centrifugal compressor and could predict the performance at design and off-design conditions using cascade data. A design procedure for radial cascade diffusers for incompressible flow, based on the maximum ratio between the flow deflection and the total pressure loss coefficient, was proposed by Pavesi et al 4 The useful design charts of a diffuser were provided and validated by the test cases, and the results had a satisfactory agreement. Rossetti et al 5 presented a multi-objective optimum design procedure aimed at achieving the best compromise between flow deflection, static pressure recovery, and total pressure loss for aerodynamic diffusers.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Pampreen 3 provided some results from experience with the use of a cascade in the design of diffuser for the centrifugal compressor and could predict the performance at design and off-design conditions using cascade data. A design procedure for radial cascade diffusers for incompressible flow, based on the maximum ratio between the flow deflection and the total pressure loss coefficient, was proposed by Pavesi et al 4 The useful design charts of a diffuser were provided and validated by the test cases, and the results had a satisfactory agreement. Rossetti et al 5 presented a multi-objective optimum design procedure aimed at achieving the best compromise between flow deflection, static pressure recovery, and total pressure loss for aerodynamic diffusers.…”
Section: Introductionmentioning
confidence: 99%
“…A design procedure for radial cascade diffusers for incompressible flow, based on the maximum ratio between the flow deflection and the total pressure loss coefficient, was proposed by Pavesi et al. 4 The useful design charts of a diffuser were provided and validated by the test cases, and the results had a satisfactory agreement. Rossetti et al.…”
Section: Introductionmentioning
confidence: 99%