| contributor author | S. Gilham | |
| contributor author | P. C. Ivey | |
| contributor author | J. M. Owen | |
| date accessioned | 2017-05-08T23:38:26Z | |
| date available | 2017-05-08T23:38:26Z | |
| date copyright | April, 1992 | |
| date issued | 1992 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26699#268_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/110236 | |
| description abstract | Self-induced flow occurs when a tube, open at one end and sealed at the other, is rotated about its central axis: Fluid flows along the axis from the open end toward the sealed end and returns in a layer adjacent to the inner surface of the tube. This mechanism, which can occur under isothermal or nonisothermal conditions, is believed to be responsible for the so-called “hot-poker effect” that was observed during anti-icing tests on the nose bullet of an aeroengine. This paper describes a combined theoretical and experimental study of self-induced flow. It is shown that, for the length-to-diameter (L/D) ratios and rotational Reynolds numbers associated with the anti-icing tubes of aeroengines, the laminar flow near the sealed end of the tube is similar to that of the so-called free disk. Swirl in the air outside the open end reduces the self-induced flow, but flow can reach the sealed end of a stepped tube that has either a sudden contraction or a sudden enlargement. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Self-Induced Flow in a Stepped Rotating Tube | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906583 | |
| journal fristpage | 268 | |
| journal lastpage | 274 | |
| identifier eissn | 0742-4795 | |
| keywords | Flow (Dynamics) | |
| keywords | Laminar flow | |
| keywords | Reynolds number | |
| keywords | Disks | |
| keywords | Bullets | |
| keywords | Mechanisms AND Fluid dynamics | |
| tree | Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002 | |
| contenttype | Fulltext | |