| contributor author | R. J. Goldstein | |
| contributor author | E. R. G. Eckert | |
| contributor author | J. W. Ramsey | |
| date accessioned | 2017-05-09T00:05:45Z | |
| date available | 2017-05-09T00:05:45Z | |
| date copyright | October, 1968 | |
| date issued | 1968 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26671#384_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/125734 | |
| description abstract | An experimental investigation has been conducted to determine the film cooling effectiveness with injection of air through a discrete hole into a turbulent boundary layer of air on a flat plate. The secondary air enters at either an angle of 35 deg or an angle of 90 deg to the main flow. The film cooling effectiveness is found to be considerably different from that obtained in previous studies in which the secondary fluid was introduced through a continuous slot. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Film Cooling With Injection Through Holes: Adiabatic Wall Temperatures Downstream of a Circular Hole | |
| type | Journal Paper | |
| journal volume | 90 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3609223 | |
| journal fristpage | 384 | |
| journal lastpage | 393 | |
| identifier eissn | 0742-4795 | |
| keywords | Cooling | |
| keywords | Wall temperature | |
| keywords | Flow (Dynamics) | |
| keywords | Fluids | |
| keywords | Boundary layer turbulence AND Flat plates | |
| tree | Journal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 004 | |
| contenttype | Fulltext | |
