2017
DOI: 10.1016/j.energy.2017.06.067
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Effect of inter-stage phenomena on the performance prediction of two-stage turbocharging systems

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Cited by 17 publications
(4 citation statements)
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“…Galindo et al 29 investigated the performance of the two-stage turbocharging approach, and the results presented that the overall performance of the 2ST system for the entire operative range and characterized the optimum control of the components for various operating conditions. Avola et al 30 investigated the accuracy of performance measurement in two-stage turbocharging systems in the context of aerothermal interstage phenomena and concluded that the turbine net efficiency was reduced by about 10% at elevated corrected mass flow operations. The 2ST is also adopted at high altitudes or in flight, as it can offer a high compression pressure ratio.…”
Section: Introductionmentioning
confidence: 99%
“…Galindo et al 29 investigated the performance of the two-stage turbocharging approach, and the results presented that the overall performance of the 2ST system for the entire operative range and characterized the optimum control of the components for various operating conditions. Avola et al 30 investigated the accuracy of performance measurement in two-stage turbocharging systems in the context of aerothermal interstage phenomena and concluded that the turbine net efficiency was reduced by about 10% at elevated corrected mass flow operations. The 2ST is also adopted at high altitudes or in flight, as it can offer a high compression pressure ratio.…”
Section: Introductionmentioning
confidence: 99%
“…Today, the receipt of new data on the features of gas-dynamics and heat transfer in gas-air tracts of turbocharged engines is an important task, since the efficiency of power machines based on ICEs depends on the perfection of these processes [1][2][3]. Modern research in this field is devoted to the study of the parameters of gas flows at the inlet and outlet of the TC turbine [4][5][6], heat transfer inside the compressor [7], the thermal effect of the turbine on the compressor in the composition of the TC [8] and ways to improve the efficiency of the turbocharger [9,10].…”
Section: Introductionmentioning
confidence: 99%
“…The compressor was isolated from the engine inlet to work against a compressor back pressure valve (CBPV). The setup was used to observe certain unsteady flow TC behaviors [24] [25], and used to improve 1D modeling accuracies [26] [27] and identify the effect of modifying the positions of intercooler on a 2 stage boosting system [28]. Although similar engine gas stand (EGS) rigs are in operation globally, there are a few important features to note here that allows the study of complex air handling systems.…”
Section: Introductionmentioning
confidence: 99%
“…Although similar engine gas stand (EGS) rigs are in operation globally, there are a few important features to note here that allows the study of complex air handling systems. The facility discussed in this paper is the next generation of the facility discussed in reference [24] to [28] which had difficulties measuring turbine-side flow.…”
Section: Introductionmentioning
confidence: 99%