| contributor author | M. Y. Jabbari | |
| contributor author | R. J. Goldstein | |
| date accessioned | 2017-05-08T23:04:44Z | |
| date available | 2017-05-08T23:04:44Z | |
| date copyright | April, 1978 | |
| date issued | 1978 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26740#303_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91003 | |
| description abstract | Results of an experimental investigation of film cooling and heat transfer following injection through two staggered rows of holes are reported. The two staggered rows are considerably more effective in protecting the wall than a single row. The film cooling effectiveness at locations beyond about 30-hole dia downstream of injection is laterally uniform. The heat transfer coefficient is within a few percent of that without injection at low blowing rates, but it increases rapidly as the blowing rate increases above unity. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Adiabatic Wall Temperature and Heat Transfer Downstream of Injection Through Two Rows of Holes | |
| type | Journal Paper | |
| journal volume | 100 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446350 | |
| journal fristpage | 303 | |
| journal lastpage | 307 | |
| identifier eissn | 0742-4795 | |
| keywords | Heat transfer | |
| keywords | Wall temperature | |
| keywords | Cooling AND Heat transfer coefficients | |
| tree | Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002 | |
| contenttype | Fulltext | |