| contributor author | D. K. Mukherjee | |
| date accessioned | 2017-05-08T23:00:32Z | |
| date available | 2017-05-08T23:00:32Z | |
| date copyright | October, 1976 | |
| date issued | 1976 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26728#554_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/88550 | |
| description abstract | The pressure loss coefficient of an impingement cooled system similar to that often used to cool the leading edge of a turbine blade has been determined from model test. The influence of Reynolds number in the range tested is negligible. However, the influence of relative distance of the jet holes from the surface to be cooled is very significant. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Pressure Loss Coefficient of Impingement Cooled Leading Edge System of a Turbine Blade | |
| type | Journal Paper | |
| journal volume | 98 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446236 | |
| journal fristpage | 554 | |
| journal lastpage | 556 | |
| identifier eissn | 0742-4795 | |
| keywords | Pressure | |
| keywords | Turbine blades AND Reynolds number | |
| tree | Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004 | |
| contenttype | Fulltext | |
