| contributor author | S. H. Bhavnani | |
| contributor author | J. Waggott | |
| contributor author | J. M. Khodadadi | |
| contributor author | J. S. Goodling | |
| date accessioned | 2017-05-08T23:39:57Z | |
| date available | 2017-05-08T23:39:57Z | |
| date copyright | April, 1992 | |
| date issued | 1992 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28619#454_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111111 | |
| description abstract | Results are presented for an experimental study of fluid flow in models of gas turbine disk cavities. Experiments were performed on 70-cm-dia disks for rotational Reynolds numbers up to 2.29 × 106 . Velocity and pressure distributions are presented and compared to previous theoretical and experimental studies for a free disk, and an unshrouded plane Rotor–Stator disk system. Minimum coolant flow rates for the prevention of ingress, determined for the case of a simple axial rim seal, compare well with previously published data. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | An Experimental Study of Fluid Flow in Disk Cavities | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2929165 | |
| journal fristpage | 454 | |
| journal lastpage | 461 | |
| identifier eissn | 1528-8900 | |
| keywords | Fluid dynamics | |
| keywords | Disks | |
| keywords | Cavities | |
| keywords | Stators | |
| keywords | Pressure | |
| keywords | Flow (Dynamics) | |
| keywords | Reynolds number | |
| keywords | Coolants | |
| keywords | Gas turbines AND Rotors | |
| tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002 | |
| contenttype | Fulltext | |
