2008
DOI: 10.1016/j.ijthermalsci.2007.10.002
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Sensitivity analysis of STIG based combined cycle with dual pressure HRSG

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Cited by 24 publications
(10 citation statements)
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“…The stack temperature or HRSG exit temperature rises with increase in pressure ratio and decreases with increase in GTIT. The total change in thermal efficiency is from 41% to 48% and the specific power from 0.35 MW to 0.67 MW with the variations in pressure ratio (7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18) and temperature (1100°C -1300°C). The CO 2 emissions are changed from 0.39 kg/kWh to 0.46 kg/kWh.…”
Section: Resultsmentioning
confidence: 99%
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“…The stack temperature or HRSG exit temperature rises with increase in pressure ratio and decreases with increase in GTIT. The total change in thermal efficiency is from 41% to 48% and the specific power from 0.35 MW to 0.67 MW with the variations in pressure ratio (7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18) and temperature (1100°C -1300°C). The CO 2 emissions are changed from 0.39 kg/kWh to 0.46 kg/kWh.…”
Section: Resultsmentioning
confidence: 99%
“…The current work shows from 0.4 to 0.46 kg/kWh with the variations in pressure and temperature. Figure 4 results the performance characteristics, CO 2 emissions and stack temperature with compressor pressure ratio (7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18) and GTIT (1100°C -1300°C) for a water Comparative studies of augmentation in combined cycle power plants T. Srinivas and B. V. Reddy injected CC plant. It reveals the significant influence of water injection on thermal efficiency and specific power of the plant.…”
Section: Resultsmentioning
confidence: 99%
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“…The major exergetic loss occurs in gas turbine combustion chamber in the order of 27·5 percent and the minor exergetic loss is in deaerator. With a steam injection in combustion chamber, this major exergetic loss can be decreased (Srinivas et al , 2008. Next to GTCC, considerable level of exergy is destroyed in compressor, gas turbine, HRSG and exhaust in the range of 2 to 3 percent.…”
Section: Resultsmentioning
confidence: 99%
“…In the literature, very often one may experience two definitions of the relative steam injection coefficient: first, related to the air mass flux, k = m s5b /ṁ a (according to [6,14,24] ) and the second, related to the fuel mass flux, β =ṁ s /ṁ f (according to [16,18,21]). …”
Section: Mathematical Model In the Cfm Codementioning
confidence: 99%