SAE Technical Paper Series 2020
DOI: 10.4271/2020-01-2225
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Experimental and Numerical Investigation of a Turbocharger Turbine Using Exergy Analysis at Non-Adiabatic Conditions

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Cited by 5 publications
(6 citation statements)
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“…The use of the concept of exergy as a post-processing tool is rapidly growing in turbocharger applications [9,30,31,[40][41][42]. However, in the present work, exergy assumes an important role in the pre-processing phase, since it represents a constraint for the design of the pulses.…”
Section: Validation Studymentioning
confidence: 92%
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“…The use of the concept of exergy as a post-processing tool is rapidly growing in turbocharger applications [9,30,31,[40][41][42]. However, in the present work, exergy assumes an important role in the pre-processing phase, since it represents a constraint for the design of the pulses.…”
Section: Validation Studymentioning
confidence: 92%
“…To replicate the experimental setup, the computational domain is modified by substituting the exhaust manifold with a straight pipe 310 mm long. Adiabatic boundary conditions are imposed at the walls since, under gas-stand conditions, the expansion ratio has been demonstrated to not vary with respect to the type of boundary condition imposed [30]. Two different operating points are also studied through the DES model: the first is characterized by a similar rotational speed as for the pulsating flow cases, while the second represents an off-design point to assess the generality of the model.…”
Section: Validation Studymentioning
confidence: 99%
“…Then, a steady-state simulation is performed through the use of a multireference frame method. The walls are treated as adiabatic since, under continuous flow conditions, the expansion ratio has been demonstrated to not vary with respect to the type of boundary condition imposed [28].…”
Section: Validation Under Steady Flowmentioning
confidence: 99%
“…On the other hand, the first law of thermodynamics is not sufficient on its own to understand the aerothermodynamic behavior of the turbocharger, such as the losses caused by heat transfer and internal irreversibilities. S. M. Lim et al have performed a numerical CFD-based exergy analysis, in which the CFD results have also been validated with the experimental data, and suggested that the aerothermodynamic performance cannot be fully depicted when based on an energetic consideration alone [1]. Furthermore, S. M. Lim et al concluded that the amount of losses caused by heat transfer and internal irreversibilities occurs during the expansion process and fluctuates between factors of 8 and 15 for different operating points.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, the traditional approach via the first law of thermodynamics does not provide adequate insight into the prevalent aerothermodynamic losses. By introducing the entropy term to quantify the irreversibility The diabatic (i.e., non-adiabatic) behavior and heat transfer within the turbocharger is significant, especially at low operating speeds, as the effects of the heat transfer dominate the aerodynamic turbine expansion work, leading to overestimation of the turbine power and isentropic efficiency [1]. Therefore, the characterization of heat flows in turbochargers is of great interest beyond the state of the art.…”
Section: Introductionmentioning
confidence: 99%