Pregled bibliografske jedinice broj: 644438
Detailed analysis of the effect of the turbine and compressor isentropic efficiency on the thermal efficiency and the total entropy change of Brayton cycle
Detailed analysis of the effect of the turbine and compressor isentropic efficiency on the thermal efficiency and the total entropy change of Brayton cycle // Digital proceedings of the 8th Conference on sustainable development of energy, water and environment system / Ban, Marko ; Duić, Neven ; Guzović, Zvonimir (ur.).
Dubrovnik, 2013. (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
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Naslov
Detailed analysis of the effect of the turbine and compressor isentropic efficiency on the thermal efficiency and the total entropy change of Brayton cycle
Autori
Živić Marija ; Galović Antun ; Končić Ružica
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
Digital proceedings of the 8th Conference on sustainable development of energy, water and environment system
/ Ban, Marko ; Duić, Neven ; Guzović, Zvonimir - Dubrovnik, 2013
Skup
8th Conference on sustainable development of energy, water and environment system
Mjesto i datum
Dubrovnik, Hrvatska, 22.09.2013. - 27.09.2013
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Brayton cycle; thermal efficiency; net work per cycle; total entropy change
Sažetak
In this paper, energy and entropy analysis of the Brayton cycle with ideal gas of constant physical properties and with the specific heat ratios k = 1.3 and k=1.4 is given. Two cases with reversible (isentropic) and irreversible adiabatic processes in the turbine and compressor are considered. The cycles are analyzed in dependence of the pressure ratio p2/p1 and the ratio T3/T1 of turbine inlet temperature T3 and the compressor inlet temperature T1. Irreversibility of the adiabatic processes in the turbine and compressor is taken into account using the values of the isentropic efficiencies, for compresor 0.88 and for turbine 0.92. All relevant expressions are given in an analytical form, and results are shown in diagrams and interpreted for the values of pressure ratio in the range from 1.0 to 22.0 and the values of the temperature ratio T3/T1 = 1.5 ; 2.0 ; 3.0 ; 3.5 and 4.0.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo
POVEZANOST RADA
Projekti:
120-1201760-1757 - Izmjena topline i mase u fluidiziranom sloju
152-1201760-2202 - Numeričko modeliranje konvekcijsko difuzijskih procesa s promjenom faza (Živić, Marija, MZOS ) ( CroRIS)
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb,
Strojarski fakultet, Slavonski Brod