| contributor author | M. G. Dunn | |
| contributor author | F. J. Stoddard | |
| date accessioned | 2017-05-08T23:06:45Z | |
| date available | 2017-05-08T23:06:45Z | |
| date copyright | April, 1979 | |
| date issued | 1979 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26749#275_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/92130 | |
| description abstract | A sector of the first stage stationary inlet nozzle of the AiResearch TFE-731-2 engine was instrumented with thin-film heat-transfer gages and experiments were performed to obtain detailed heat-transfer rate distributions. It is shown that the experimental apparatus can be used to study total-pressure losses in cascades. The experimental apparatus consists of a helium-driven shock tube, as a short-duration source of high-temperature high-pressure gas, driving a nozzle-test-section mounted near the exit of a primary shock-tunnel nozzle and extending into the shock-tunnel receiver tank. The nozzle-test-section device consists of a forward transition section with a circular opening facing the supersonic primary nozzle flow and with the external shape of a frustum of a cone. Internal contouring is provided to transform the circular-section subsonic intake flow into one filling a 176 deg annular segment having a geometry approximating that of the entrance to the turbine stator stage in a turbojet. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Measurement of Heat-Transfer Rate to a Gas Turbine Stator | |
| type | Journal Paper | |
| journal volume | 101 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3446483 | |
| journal fristpage | 275 | |
| journal lastpage | 280 | |
| identifier eissn | 0742-4795 | |
| keywords | Heat transfer | |
| keywords | Gas turbines | |
| keywords | Stators | |
| keywords | Nozzles | |
| keywords | Tunnels | |
| keywords | Flow (Dynamics) | |
| keywords | Shock (Mechanics) | |
| keywords | Pressure | |
| keywords | Thin films | |
| keywords | Gages | |
| keywords | Engines | |
| keywords | Foundry coatings | |
| keywords | High pressure (Physics) | |
| keywords | Turbojets | |
| keywords | High temperature | |
| keywords | Turbines | |
| keywords | Geometry | |
| keywords | Helium | |
| keywords | Shapes AND Shock tubes | |
| tree | Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 002 | |
| contenttype | Fulltext | |
