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Micro Turbine Cycle Optimization by kawila1151 is a document available to read on EtoBox.
This paper discusses the optimization of thermodynamic cycles for an advanced micro turbine power plant, focusing on the DevJet micro jet engine. It evaluates twelve variants of the Brayton cycle by varying pressure ratios and maximum temperatures to determine optimal configurations, ultimately selecting a variant with a pressure ratio of 4.5 and a maximum temperature of 1,050 K. The results, including efficiency and mass flow data, are validated using GasTurb software to generate thermodynamic cycle diagra
- Author
- kawila1151
- Language
- EN