| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 7050443 | Applied Thermal Engineering | 2013 | 7 Pages |
Abstract
⺠Dimple-rib compound cooling technique for internal cooling of gas turbine blade is proposed. ⺠Detailed heat transfer coefficient and pressure loss measurement results are presented. ⺠The proposed compound cooling technique showed better thermal performance than rib only or dimpled only cooling technique.
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Fluid Flow and Transfer Processes
Authors
Eun Yeong Choi, Yong Duck Choi, Won Suk Lee, Jin Teak Chung, Jae Su Kwak,