| contributor author | R. E. Mayle | |
| contributor author | M. F. Blair | |
| contributor author | D. A. Bailey | |
| contributor author | F. C. Kopper | |
| date accessioned | 2017-05-08T23:02:50Z | |
| date available | 2017-05-08T23:02:50Z | |
| date copyright | January, 1977 | |
| date issued | 1977 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26730#77_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/89848 | |
| description abstract | The effects of streamline curvature on film cooling effectiveness are discussed. Experiments for air discharged through a slot and into a turbulent boundary layer along a flat, convex, and concave surface are described. Adiabatic wall effectiveness measurements on each surface for several blowing rates are presented. Boundary-layer velocity and temperature measurements are also presented for one of the blowing rates. Compared to the results for the flat surface, convex curvature is found to increase the adiabatic wall effectiveness whereas concave curvature is found to be detrimental. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Streamline Curvature on Film Cooling | |
| type | Journal Paper | |
| journal volume | 99 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446255 | |
| journal fristpage | 77 | |
| journal lastpage | 82 | |
| identifier eissn | 0742-4795 | |
| keywords | Cooling | |
| keywords | Measurement | |
| keywords | Temperature measurement | |
| keywords | Boundary layers AND Boundary layer turbulence | |
| tree | Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001 | |
| contenttype | Fulltext | |
