2020
DOI: 10.1115/1.4047781
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A Discrete Adjoint Method for Two-Phase Condensing Flows Applied to the Shape Optimization of Turbine Cascades

Abstract: Abstract This paper presents a fully turbulent two-phase discrete adjoint method for metastable condensing flows targeted to turbomachinery applications. The method is based on a duality preserving algorithm and implemented in the open-source CFD tool SU2. The optimization framework is applied to the shape optimization of two canonical steam turbine cascades, commonly referred to as White cascade and Dykas cascade. The optimization were carried out by minimizing … Show more

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(1 citation statement)
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“…Later it was studied on the supersonic flight due to the characteristic mist Mach cone formation or in the hypersonic wind tunnels operation (Wegener;Mack, 1958). Also, this phenomenon have been of interest for some vapour handling process, because it can affect the equipment behaviour as the case of supersonic ejectors (Yang et al, 2019), compressors (Lettieri et al, 2015) and turbines (Pini et al, 2020). Since, in this case the condensation shock can be undesirable due to the irreversibility that this phenomenon generates due to condensation itself and the possible oblique shock waves production.…”
Section: Condensation Shockmentioning
confidence: 99%
“…Later it was studied on the supersonic flight due to the characteristic mist Mach cone formation or in the hypersonic wind tunnels operation (Wegener;Mack, 1958). Also, this phenomenon have been of interest for some vapour handling process, because it can affect the equipment behaviour as the case of supersonic ejectors (Yang et al, 2019), compressors (Lettieri et al, 2015) and turbines (Pini et al, 2020). Since, in this case the condensation shock can be undesirable due to the irreversibility that this phenomenon generates due to condensation itself and the possible oblique shock waves production.…”
Section: Condensation Shockmentioning
confidence: 99%