| contributor author | D. J. Mee | |
| contributor author | N. C. Baines | |
| contributor author | M. L. G. Oldfield | |
| date accessioned | 2017-05-08T23:40:00Z | |
| date available | 2017-05-08T23:40:00Z | |
| date copyright | January, 1992 | |
| date issued | 1992 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28617#163_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111135 | |
| description abstract | The boundary layers of a transonic turbine blade have been measured in detail. The full velocity profiles have been measured at a number of stations on both the suction and pressure surfaces, at conditions representative of engine operation, using a Pilot traverse technique and a large-scale (300 mm chord) linear cascade. This information has made it possible to follow the development of the boundary layers, initially laminar, through a region of natural transition to a fully developed turbulent layer. Comparisons with other, less detailed, measurements on the same profile using Pilot traverse and surface-mounted thin films confirm the essential features of the boundary layers. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Detailed Boundary Layer Measurements on a Transonic Turbine Cascade | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927980 | |
| journal fristpage | 163 | |
| journal lastpage | 172 | |
| identifier eissn | 1528-8900 | |
| keywords | Measurement | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Boundary layers | |
| keywords | Turbines | |
| keywords | Chords (Trusses) | |
| keywords | Pressure | |
| keywords | Thin films | |
| keywords | Turbulence | |
| keywords | Suction | |
| keywords | Engines AND Turbine blades | |
| tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001 | |
| contenttype | Fulltext | |