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Session: Session 3A: Turbine Nozzles Simulations
Session starts: Monday 09 September, 16:00
Presentation starts: 16:20
Room: Olympia

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Tao Chen ()
Peter Newton ()
Miles Robertson ()
Ricardo Martinez-Botas ()

Abstract:
The Organic Rankine Cycle (ORC) is a technology facilitating the generation of useful mechanical power, from a wide variety of low-temperature heat sources. The specific application considered in this paper is heavy-duty vehicles, as part of a secondary (or bottoming) cycle. A single stage high-expansion-ratio turbine is a suitable type of expander for this application, the nozzle would be transonic given the high expansion ratios. This paper analyses the loss generation mechanisms within the transonic nozzle, with a view towards improving the design of high-pressure ratio turbine expanders for an increasing stage efficiency. This paper simulates the transonic flow of R1233zd(E) in a linear nozzle blade cascade by means of Computational Fluid Dynamics (CFD). The cascade is designed to achieve a uniform outlet flow Mach number of 2. An initial analysis uses irreversible entropy generation rate to study and explain the loss generating mechanisms in the nozzle under on- and off-design conditions, and the entropy loss coefficient is used to quantitively analyse the loss distribution. The loss generated in the expansion process takes 28.2 % of the overall loss, and the loss in the region after expansion takes the remaining 71.8 %. The impact of real-gas properties is then considered by comparing with an equivalent air cascade. The loss generated in the expansion process for the R1233zd(E) cascade is 19.7 % larger than that for air due to a larger non-ideal expansion loss. The loss generated in the region after the expansion process for the R1233zd(E) cascade is 11.4 % lower than that for air due to a lower loss caused by trailing-edge wave and trailing-edge wake. The overall loss is 4.4 % lower in the R1233zd(E) cascade; conversely, the total pressure loss coefficient is 13.8 % larger in the R1233zd(E) cascade than that in the air cascade. This is explained by an analysis of Gibbs entropy formula for a real-gas which shows that the stagnation pressure loss is attributed to both an entropy gain and a real gas effect.