| contributor author | Schreivogel, Peter | |
| contributor author | Pfitzner, Michael | |
| date accessioned | 2017-05-09T01:34:03Z | |
| date available | 2017-05-09T01:34:03Z | |
| date issued | 2016 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_138_03_031003.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/162746 | |
| description abstract | A new approach for steadystate heat transfer measurements is proposed. Temperature distributions are measured at the surface and a defined depth inside the wall to provide boundary conditions for a threedimensional heat flux calculation. The practical application of the technique is demonstrated by employing a superposition method to measure heat transfer and film cooling effectiveness downstream of two different 0.75D deep narrow trench geometries and cylindrical holes. Compared to the cylindrical holes, both trench geometries lead to an augmentation of the heat transfer coefficient supposedly caused by the highly turbulent attached cooling film emanating from the trenches. Areas of high heat transfer are visible, where recirculation bubbles or large amounts of coolant are expected. Increasing the density ratio from 1.33 to 1.60 led to a slight reduction of the heat transfer coefficient and an increased cooling effectiveness. Both trenches provide a net heat flux reduction (NHFR) superior to that of cylindrical holes, especially at the highest momentum flux ratios. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Heat Transfer Measurements Downstream of Trenched Film Cooling Holes Using a Novel Optical Two Layer Measurement Technique | |
| type | Journal Paper | |
| journal volume | 138 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4031919 | |
| journal fristpage | 31003 | |
| journal lastpage | 31003 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 003 | |
| contenttype | Fulltext | |