2017
DOI: 10.1115/1.4037029
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Effects of Coolant Density, Specific Heat Capacity, and Biot Number on Turbine Vane Cooling Effectiveness

Abstract: This paper describes the effects of coolant-to-mainstream density ratio and specific heat capacity flux ratio (the product of blowing ratio and specific heat capacity ratio) on the overall cooling effectiveness of high pressure (HP) turbine vanes. Experimental measurements have been conducted at correct engine-matched conditions of Mach number, Reynolds number, turbulence intensity, and coolant-to-mainstream momentum flux ratio. Vanes tested were fully cooled production parts from an engine currently in servic… Show more

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Cited by 11 publications
(4 citation statements)
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“…Due to the effect of the temperature on physical properties, the accuracy of the results will be inevitably affected while using the similarity criterion. Luque et al (2016Luque et al ( , 2017aLuque et al ( , 2017b used a new temperature parameter to define the OCE and expanded the hypothesis theory, which was verified by the experiments.…”
Section: Introductionmentioning
confidence: 83%
“…Due to the effect of the temperature on physical properties, the accuracy of the results will be inevitably affected while using the similarity criterion. Luque et al (2016Luque et al ( , 2017aLuque et al ( , 2017b used a new temperature parameter to define the OCE and expanded the hypothesis theory, which was verified by the experiments.…”
Section: Introductionmentioning
confidence: 83%
“…The density of each tested lubricant was measured as specified by ASTM standard D4052, to identify the mass per unit volume, which impacts its ability to deliver lubrication and dissipate the heat [31]. A pycnometer was used to calculate the ratio of weight-to-volume at 15°C to obtain the density data.…”
Section:  Densitymentioning
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.…”
Section: Nomenclaturementioning
confidence: 99%
“…These nodes are solved using Eqs. (3)(4)(5), respectively. The simulation parameters are listed in Table 2.…”
Section: Modelingmentioning
confidence: 99%