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Abstract
Partial-evaporation organic Rankine cycle power systems are a promising technology for power generation from lowtemperature heat sources, such as waste heat and geothermal heat. A specific challenge in two-phase turbines is converging diverging nozzle design and performance analysis. Existing one dimensional methods for two-phase flows in nozzles typically rely on space-marching approaches, which are unsuitable for predicting shock waves and thus limit their application to adapted expansion conditions. To address the limitations of existing models, this paper presents a new one-dimensional two-phase flow model suitable for capturing shockwaves in converging-diverging nozzles. The model employs a finite volume method to solve the balance equations in a conservative form, using time marching methods to reach the steady-state solution. The predictive performance of the proposed model is validated against experimental data from converging-diverging nozzles using various working fluids, including organic molecules and CO2. The results indicate that the proposed model formulation is suitable for predicting the performance of two-phase nozzles in terms of pressure distribution, critical mass flow rate, and shock wave characteristics across a wide range of operating conditions. These findings suggest that the developed model can be a reliable tool for the preliminary design and analysis of converging-diverging nozzles in two-phase turbines.
Original language | English |
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Title of host publication | Proceedings of the ASME Turbo Expo 2025 |
Number of pages | 14 |
Publisher | The American Society of Mechanical Engineers (ASME) |
Publication status | Accepted/In press - 2025 |
Event | ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition - Memphis, United States Duration: 16 Jun 2025 → 20 Jun 2025 |
Conference
Conference | ASME Turbo Expo 2025 |
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Country/Territory | United States |
City | Memphis |
Period | 16/06/2025 → 20/06/2025 |
Keywords
- Organic Rankine Cycle
- Evaporation
- Shock waves
- Converging-diverging nozzle
- Space-marching methods
- Time-marching methods
- Numerical flux
Fingerprint
Dive into the research topics of 'A Hyperbolic One-Dimensional Model for Two-Phase Flows in Converging-Diverging Nozzles'. Together they form a unique fingerprint.Projects
- 2 Active
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Extension of the method of characteristics for the design oftwo-phase supersonic turbines in partial-evaporationorganic Rankine cycle systems
Cioffi, A. (PhD Student), Haglind, F. (Main Supervisor), Agromayor, R. (Supervisor), Desai, N. B. (Supervisor) & Bassi, F. (Supervisor)
01/09/2024 → 31/08/2027
Project: PhD
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Training42Phase: Next generation turbomachinery with two-phase flow
Haglind, F. (PI), Desai, N. B. (Project Manager), Persico, G. B. A. (Project Participant), Barros, A. (Project Participant), Bassi, F. (Project Participant), Schwingshackl, C. (Project Participant), Nowell, D. (Project Participant), Bergamin, A. (PhD Student), Cioffi, A. (PhD Student), Prakash Diwanji, S. (PhD Student) & He, J. (PhD Student)
01/12/2023 → 30/11/2027
Project: Research