Modeling the performance of a two-phase turbine using numerical methods and the results of nozzle, static cascade, and windage experiments
Performance models for a two-phase turbine were developed to verify the understanding of the loss mechanisms and to extrapolate from the single-nozzle test condition to a full-admission turbine. The numerical models for predicting the performance of the nozzle and the combined nozzle and rotor are described. Results from two-phase, static cascade tests and disk-friction and windage experiments are used to calibrate the performance model(s). Model predictions are compared with single-nozzle prototype-turbine test results, and extrapolations are made to a full-admission design. The modeling also provides predictions of performance for turbines with various blade geometries, inlet conditions, and droplet sizes. Thus the modeling provides insight into design improvements.
- Research Organization:
- California Univ., Livermore (USA). Lawrence Livermore Lab.
- DOE Contract Number:
- W-7405-ENG-48
- OSTI ID:
- 6565012
- Report Number(s):
- UCRL-80749; CONF-781202-15
- Resource Relation:
- Conference: ASME meeting, San Francisco, CA, USA, 10 Dec 1978
- Country of Publication:
- United States
- Language:
- English
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NOZZLES
PERFORMANCE
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TURBINES
DESIGN
DROPLETS
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GEOTHERMAL ENERGY CONVERSION
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THERMODYNAMICS
TURBINE BLADES
TWO-PHASE FLOW
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FLUID FLOW
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TURBOMACHINERY
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