Q1/ A gas turbine operates with components as shown in figure 1. Air enters this first compressor at 96.5 kPa. and 15.5°C; the pressure ratio is 3 for each stage of compression; the air temperature when entering a turbine is 504.5°C; and the heat perfect exchanger. (Take air index as 1.4 and specific heat as 1.005 kJ/kg.K). Draw T-S diagram and determine: a. The air mass flow rate, and the rates of heat addition and rejection when this produced power is 745.7 kW. b. What will be the effect of using normal heat exchanger on the thermal efficiency? Inter-cooler cc2 Cormpressors Turbines Generator set State1 Нeat Exchanger State10

Q1/ A gas turbine operates with components as shown in figure 1. Air enters this first compressor at 96.5 kPa. and 15.5°C; the pressure ratio is 3 for each stage of compression; the air temperature when entering a turbine is 504.5°C; and the heat perfect exchanger. (Take air index as 1.4 and specific heat as 1.005 kJ/kg.K). Draw T-S diagram and determine: a. The air mass flow rate, and the rates of heat addition and rejection when this produced power is 745.7 kW. b. What will be the effect of using normal heat exchanger on the thermal efficiency? Inter-cooler cc2 Cormpressors Turbines Generator set State1 Нeat Exchanger State10

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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