Volume 3: Turbo Expo 2004 2004
DOI: 10.1115/gt2004-53547
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Features of a Cooling System Simulation Tool Used in Industrial Preliminary Design Stage

Abstract: Due to expected increases in gas turbine performance, strictly related to firing temperature, heat transfer is a major issue in design processes. To keep components temperature levels below design requirements, cooling systems are commonly used. Nowadays, nozzle and blade cooling systems have reached a high degree of complexity. In a preliminary design stage, both experimental and 3D numerical analyses are usually not very suitable to define geometry, coolant mass flow rate or cooling system typology. This is … Show more

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Cited by 18 publications
(9 citation statements)
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“…The majority of previous works related to conjugate heat transfer (CHT) models (eg, Starke et al, Montenay et al, Ni et al, Heselhaus, and Sun et al) has assumed steady flow conditions to study heat transfer and flow field characteristics. However, actual flow conditions inside turbines are often variable and unsteady.…”
Section: Discussionmentioning
confidence: 99%
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“…The majority of previous works related to conjugate heat transfer (CHT) models (eg, Starke et al, Montenay et al, Ni et al, Heselhaus, and Sun et al) has assumed steady flow conditions to study heat transfer and flow field characteristics. However, actual flow conditions inside turbines are often variable and unsteady.…”
Section: Discussionmentioning
confidence: 99%
“…They used 1D simulation approaches to investigate internal cooling passages. An advantage of 1D modelling is that it is less time‐consuming compared with 3D modelling . One may use 1D modelling if they are not too strict on the accuracy of the results but expecting to have some general understanding on the heat transfer behaviour …”
Section: Modellingmentioning
confidence: 99%
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“…In order to achieve better convergence, the differences between the values of wall temperature are calculated in each iteration. The calculation is eventually stopped when the convergence criteria for this temperate difference become less than 10 25 . The details are provided in the next subsections.…”
Section: The Present Cht Solution Algorithmmentioning
confidence: 99%
“…R ESEARCH investment in metal effectiveness (or overall cooling effectiveness) measurement techniques has been driven by the desire to accurately assess the overall thermal performance of nozzle guide vanes or turbine blades at engine-realistic conditions [1][2][3][4][5][6]. The traditional approach of predicting overall thermal performance of such parts from a thermal model with boundary conditions obtained from separate experiments [7][8][9][10] has the disadvantage that errors in underlying measurements can accumulate in the final result. Additionally, certain coupling terms are inherently absent in the separated experiments, limiting the accuracy of the predicted performance, even in the absence of experimental errors.…”
Section: Nomenclaturementioning
confidence: 99%