19:49 u.51% 4ชื่อGas at 5.15 bar and 800 °C flows into theturbine and expands through the centrifugalturbine up to 1.03 bar if the Cp value is1.0.J/kg K and = 0.717 kJ/kg K. Thecompressor inlet air temperature is 30'CCalculate 1.Temperature exhaust from theturbine. 2. Net work producedGIF12379.ค ต จ ข ชร น ย บ ล* M L, 1.ฟ ห ก ด เ4 W 1 bb a?123ไทยa

A gas turbine cycle works on the principle of the Brayton thermal cycle. It consists of two constant…

Answered: Gas at 5.15 bar and 800 °C flows into…

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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hi At the beginning of the compression process of an air standard Otto cycle, p1 = 1 bar, T1 = 300 K. The maximum temperature in the cycle is 2250 K and the compression ratio is 9.8. The engine has 4 cylinders and an engine displacement of Vd = 2.6 L. Determine per cylinder: Only letters d,e, and f needed a) the volume at state 1.b) the air mass per cycle.c) the heat addition per cycle, in kJ.d) the heat rejection per cycle, in kJ. - <e) the net work per cycle, in kJ. - <f) the thermal efficiency. - <
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At the beginning of the compression process of an air standard Otto cycle, p1 = 1 bar, T1 = 300 K. The maximum temperature in the cycle is 2250 K and the compression ratio is 9.8. The engine has 4 cylinders and an engine displacement of Vd = 2.2 L. Determine per cylinder: a) the volume at state 1.b) the air mass per cycle.c) the heat addition per cycle, in kJ.

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Gas at 5.15 bar and 800 °C flows into the turbine and expands through the centrifugal turbine up to 1.03 bar if the Cp value is 1.0.J/kg K and = 0.717 kJ/kg K. The compressor inlet air temperature is 30'C Calculate 1.Temperature exhaust from the turbine. 2. Net work produced