| contributor author | Ledezma, Gustavo A. | |
| contributor author | Bunker, Ronald S. | |
| date accessioned | 2017-05-09T01:24:19Z | |
| date available | 2017-05-09T01:24:19Z | |
| date issued | 2015 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_137_01_011002.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/159870 | |
| description abstract | This article presents a geometric optimization study to maximize the total heat transfer rate between an array of discrete pin fins and the surrounding serpentine cooling flow. The fins are installed on the tip cap underside of a highpressure turbine blade (HPTB) model. The study has three parts. In the first, the numerical model is validated against experimental data obtained with liquid crystal thermography. In the second part, the heat and fluid flow performance of the pin fin assembly is simulated numerically, using RANS turbulence models in the range 25,000 < Re < 100,000 and Pr ∼ 0.7. The effect of varying the spacing and the tip cap boundary condition is investigated. In the last part of the study, it is shown that the optimal spacing between the pin fins can be correlated following the same theoretical arguments derived in the previous investigations that used simpler geometries. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Optimal Distribution of Pin Fins for Blade Tip Cap Underside Cooling | |
| type | Journal Paper | |
| journal volume | 137 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4028290 | |
| journal fristpage | 11002 | |
| journal lastpage | 11002 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 001 | |
| contenttype | Fulltext | |