2009
DOI: 10.3795/ksme-b.2009.33.7.541
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A Numerical Study of the Turbulent Flow Characteristics in the Inlet Transition Square Duct Based on Roof Configuration

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Cited by 6 publications
(6 citation statements)
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“…Although it is usually impossible to get Reynolds similarity exactly between the prototype and the model, it is well known that the turbulent flow pattern does not change any more by increasing the Reynolds number larger than 1×10 4 [7]. In this experimental condition of maximum flow, the Reynolds number is in the range of 1.2~6.1×10 5 and this means that Reynolds similarity is relatively well kept in this experiment. In addition, considering the swirl behavior in the real gas flow through the HRSG, a swirler is attached at the entrance of the model.…”
Section: Cold Flow Wind Tunnel Testsmentioning
confidence: 75%
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“…Although it is usually impossible to get Reynolds similarity exactly between the prototype and the model, it is well known that the turbulent flow pattern does not change any more by increasing the Reynolds number larger than 1×10 4 [7]. In this experimental condition of maximum flow, the Reynolds number is in the range of 1.2~6.1×10 5 and this means that Reynolds similarity is relatively well kept in this experiment. In addition, considering the swirl behavior in the real gas flow through the HRSG, a swirler is attached at the entrance of the model.…”
Section: Cold Flow Wind Tunnel Testsmentioning
confidence: 75%
“…The pressure drop was calculated as source term added in the momentum equation [13]. Number of Transfer Unit (NTU) model was used to calculate the heat transfer in the tube zone and the fan swirl velocity modelling was employed to express the swirl flow from the gas turbine [5]. Inlet conditions of the exhaust gas were summarized in Table 5 and input values to express the pressure and temperature drop at the tube zone were decided based on data of the pressure and temperature in the Ulsan combined cycle power plant unit 2 as shown in Table 6[3].…”
Section: Cfd Simulationmentioning
confidence: 99%
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“…Nu mber of Transfer Un it (NTU) model was used to calculate the heat transfer in the tube zone. Fan swirl velocity modelling was employed to express the swirl flow fro m the gas turbine [19]. Heat transfer fro m the hot gas to the wall is described by convective heat transfer.…”
Section: Cfd Modelmentioning
confidence: 99%
“…Yoo et al [13] considered the change of inlet duct shape for the improved uniform flow and showed its possibility. Ameri and Jazini [14] considered the CFD modeling of heat recovery steam generator inlet duct.…”
Section: Introductionmentioning
confidence: 99%