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• W2756080097 abstract "Abstract At the trailing edge of supersonic high-pressure turbine vanes, a typical shock pattern, the so-called fish-tail shocks, originates due to the flow rotation imposed by its finite thickness. In addition, shock and shock/fan systems can arise in case of a post-expanded channel design or at off-design conditions. ORC turbine stator blades are particularly prone to this phenomena since they are designed to provide a high outlet Mach number, especially at the first stage. In the close proximity of the saturation curve, near the critical point, molecularly complex organic fluids for ORC applications may exhibit a number of non-ideal gasdynamic effects, including a remarkable dependency of the shock properties on the upstream thermodynamic state of the fluid, at a fixed upstream Mach number. The influence of thermodynamic conditions on the shock pattern is assessed as a function of the flow deviation and compared against the ideal gas case, for which the shock properties depends on the upstream Mach number only. Non-ideal effects are investigated here using siloxane vapor MDM (Octamethyltrisiloxane, C 8 H 24 O 2 Si 3 ), as an exemplary organic fluid. The present results can be arguably extended to most vapors currently employed in ORC applications." @default.
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• W2756080097 date "2017-09-01" @default.
• W2756080097 modified "2023-09-23" @default.
• W2756080097 title "Non-ideal effects on the typical trailing edge shock pattern of ORC turbine blades" @default.
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• W2756080097 doi "https://doi.org/10.1016/j.egypro.2017.09.231" @default.
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