| contributor author | H. P. Hodson | |
| date accessioned | 2017-05-08T23:20:18Z | |
| date available | 2017-05-08T23:20:18Z | |
| date copyright | January, 1985 | |
| date issued | 1985 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26614#127_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/99881 | |
| description abstract | The state of the boundary layers near the leading edge of a high-speed turbine blade has been investigated, in cascade, using an array of surface-mounted, constant-temperature, hot-film anemometers. The measurements are interpreted with the aid of inviscid and viscous prediction codes. The effects of Reynolds number, compressibility, incidence, and free-stream turbulence are described. In all cases, the initial development of the boundary layers was extremely complex and, even at design conditions, separation and reattachment, transition and relaminarization were found to occur. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Boundary-Layer Transition and Separation Near the Leading Edge of a High-Speed Turbine Blade | |
| type | Journal Paper | |
| journal volume | 107 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239672 | |
| journal fristpage | 127 | |
| journal lastpage | 134 | |
| identifier eissn | 0742-4795 | |
| keywords | Separation (Technology) | |
| keywords | Turbine blades | |
| keywords | Boundary layers | |
| keywords | Design | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Compressibility | |
| keywords | Temperature | |
| keywords | Measurement | |
| keywords | Turbulence AND Reynolds number | |
| tree | Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001 | |
| contenttype | Fulltext | |
