Influence of Excitation Frequency, Phase Shift, and Duty Cycle on Cooling Ratio in a Dynamically Forced Impingement Jet ArraySource: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 005DOI: 10.1115/1.4046616Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The cooling ratio on a dynamically forced 7 × 7 impingement jet array is studied experimentally. The current study is focused on determining the influence of a phase shift between every row of nozzles as well as the impact of a duty cycle variation on the cooling ratio. Both parameters are studied in dependency of the impingement distance (H/D = 2, 3, 5), the (nozzle-) Reynolds-number (ReD = 3200, 5200, 7200), and the excitation frequency (f = 0 Hz − 1000 Hz). For every set of parameters, the phase shift between every row of nozzles is varied between Φ=0% and 90%, while the variation of the duty cycle is performed between duty cycle (DC) = 35% and 65%. During all investigations, the dimensionless distance between adjacent nozzles is fixed at Sx/D = Sy/D = 5, and liquid crystal thermography is used to acquire the wall temperatures, which are further processed to calculate the local Nusselt numbers. Generally, the implementation of an excitation frequency allows a case-depending increase in the cooling ratio of up to 52%. Further implementation of a phase shift yields an additional frequency-depending improvement of the cooling ratio. In case of duty cycle variation, the best case revealed an additional 19% improvement in the cooling ratio.
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| contributor author | Berthold, Arne | |
| contributor author | Haucke, Frank | |
| date accessioned | 2022-02-04T14:45:35Z | |
| date available | 2022-02-04T14:45:35Z | |
| date copyright | 2020/03/30/ | |
| date issued | 2020 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_142_5_051001.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4274315 | |
| description abstract | The cooling ratio on a dynamically forced 7 × 7 impingement jet array is studied experimentally. The current study is focused on determining the influence of a phase shift between every row of nozzles as well as the impact of a duty cycle variation on the cooling ratio. Both parameters are studied in dependency of the impingement distance (H/D = 2, 3, 5), the (nozzle-) Reynolds-number (ReD = 3200, 5200, 7200), and the excitation frequency (f = 0 Hz − 1000 Hz). For every set of parameters, the phase shift between every row of nozzles is varied between Φ=0% and 90%, while the variation of the duty cycle is performed between duty cycle (DC) = 35% and 65%. During all investigations, the dimensionless distance between adjacent nozzles is fixed at Sx/D = Sy/D = 5, and liquid crystal thermography is used to acquire the wall temperatures, which are further processed to calculate the local Nusselt numbers. Generally, the implementation of an excitation frequency allows a case-depending increase in the cooling ratio of up to 52%. Further implementation of a phase shift yields an additional frequency-depending improvement of the cooling ratio. In case of duty cycle variation, the best case revealed an additional 19% improvement in the cooling ratio. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Influence of Excitation Frequency, Phase Shift, and Duty Cycle on Cooling Ratio in a Dynamically Forced Impingement Jet Array | |
| type | Journal Paper | |
| journal volume | 142 | |
| journal issue | 5 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4046616 | |
| page | 51001 | |
| tree | Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 005 | |
| contenttype | Fulltext |