| contributor author | C. A. Hale | |
| contributor author | M. W. Plesniak | |
| contributor author | S. Ramadhyani | |
| date accessioned | 2017-05-09T00:03:38Z | |
| date available | 2017-05-09T00:03:38Z | |
| date copyright | July, 2000 | |
| date issued | 2000 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28679#553_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/124475 | |
| description abstract | The adiabatic, steady-state liquid crystal technique was used to measure surface adiabatic film cooling effectiveness values in the near-hole region (X/D<10). A parametric study was conducted for a single row of short holes (L/D≤3) fed by a narrow plenum (H/D=1). Film cooling effectiveness values are presented and compared for various L/D ratios (0.66 to 3.0), three different blowing ratios (0.5, 1.0, and 1.5), two different plenum feed configurations (co-flow and counterflow), and two different injection angles (35 and 90 deg). Injection hole geometry and plenum feed direction were found to affect short hole film cooling performance significantly. Under certain conditions, similar or improved coverage was achieved with 90 deg holes compared with 35 deg holes. This result has important implications for manufacturing of thin-walled film-cooled blades or vanes. [S0889-504X(00)00603-6] | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Film Cooling Effectiveness for Short Film Cooling Holes Fed by a Narrow Plenum | |
| type | Journal Paper | |
| journal volume | 122 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.1303705 | |
| journal fristpage | 553 | |
| journal lastpage | 557 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) AND Cooling | |
| tree | Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003 | |
| contenttype | Fulltext | |
