The literature introduced binary Brayton cycle and the isothermal concept as two promising methods used to enhance the performance of the gas turbine. Consequently, this work presents a cycle based on the blending of the two methods. This cycle is composed of gas turbine topping cycle with isothermal combustion and air turbine bottoming cycle with isothermal heating. Different parameters affecting the cycle performance have been studied. Simulations demonstrate that the present cycle achieves drastic enhancement in performance. The cycle merits justify its potential utilization for future power generation.
Abd El-Maksoud, R. (2013). Binary Brayton Cycle with Isothermal Concept. International Conference on Aerospace Sciences and Aviation Technology, 15(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013), 1-11. doi: 10.21608/asat.2013.22184
MLA
R. M. Abd El-Maksoud. "Binary Brayton Cycle with Isothermal Concept". International Conference on Aerospace Sciences and Aviation Technology, 15, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013, 2013, 1-11. doi: 10.21608/asat.2013.22184
HARVARD
Abd El-Maksoud, R. (2013). 'Binary Brayton Cycle with Isothermal Concept', International Conference on Aerospace Sciences and Aviation Technology, 15(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013), pp. 1-11. doi: 10.21608/asat.2013.22184
VANCOUVER
Abd El-Maksoud, R. Binary Brayton Cycle with Isothermal Concept. International Conference on Aerospace Sciences and Aviation Technology, 2013; 15(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013): 1-11. doi: 10.21608/asat.2013.22184
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