2012
DOI: 10.1016/j.applthermaleng.2011.09.012
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Analysis of water droplet evaporation in a gas turbine inlet fogging process

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Cited by 46 publications
(31 citation statements)
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“…(5) and (15). There remains no liquid droplet after completion evaporation of the liquid water droplets and, then, dry compression begins at state 2.…”
Section: System Analysismentioning
confidence: 99%
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“…(5) and (15). There remains no liquid droplet after completion evaporation of the liquid water droplets and, then, dry compression begins at state 2.…”
Section: System Analysismentioning
confidence: 99%
“…Performance specifications of gas turbines show that the reduced inlet temperature increases the capacity and reduces the heat transfer rate. Many researchers [6][7][8][9][10][11][12][13][14][15] have conducted experimental or analytical studies on the inlet fogging in gas turbine engines, and achieved significant improvement at various aspects of the technology including the methods of generating, controlling, and measuring water sprays as well as the non-equilibrium modeling of the transient fogging process.…”
Section: Introductionmentioning
confidence: 99%
“…In this study, a water droplet cooling technique or (water mist cooling technique) were developed by suspending fine water droplets into the working fluid. The water mist techniques, not a new cooling concept and has been successfully applied in many industrial applications [13][14][15][16][17][18]. Utilizing water mist as a cooling medium provides excellent cooling approaches to dissipate heat even larger than the single-phase air cooling approaches.…”
Section: Introductionmentioning
confidence: 99%
“…Then we expect f 3 = D 3 = 0. On the contrary, when water injection ratio f 0 is higher than f 0c , the air becomes saturated and remained liquid water droplets leave the compressor along with air [14]. In this work the analysis is restricted to the cases of complete evaporation of injected droplets inside a compressor.…”
Section: System Analysismentioning
confidence: 99%
“…Performance specifications of gas turbines show that the reduced inlet temperature increases the capacity and reduce the heat transfer rate. Many researchers as Chaker et al [6][7][8], Utamura [9], Bhargava and Mehr-Homji [10], Belarbi et al [11], Yang et al [12], Farzaneh-Gord and Deymi-Dashtebayaz [13], and Kim et al [14] have conducted experimental or analytical studies on the inlet fogging in gas turbine engines, and achieved significant improvement at various aspects of the technology including methods of generating, controlling, and measuring sprays as well as the non-equilibrium modeling of the transient fogging process.…”
Section: Introductionmentioning
confidence: 99%