Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor
October 1979
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| Format: | Technical Report |
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Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1979]
2016
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| Online Access: | http://hdl.handle.net/1721.1/104424 |
| _version_ | 1811076780280250368 |
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| author | Tan, Choon Sooi |
| author2 | Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory Tan, Choon Sooi |
| author_sort | Tan, Choon Sooi |
| collection | MIT |
| description | October 1979 |
| first_indexed | 2024-09-23T10:27:21Z |
| format | Technical Report |
| id | mit-1721.1/104424 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T10:27:21Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1979] |
| record_format | dspace |
| spelling | mit-1721.1/1044242019-04-12T16:13:10Z Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor 3-D incompressible and compressible Beltrami flow through a highly-loaded isolated rotor Tan, Choon Sooi Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory TJ778.M41 G24 no.147 Turbomachines -- Blades Compressors Vortex-motion Viscous flow October 1979 Includes bibliographical references (pages 78-79) An analysis is proposed for the three-dimensional incompressible and compressible Beltrami flow through a heavily loaded isolated rotor. It is found that, in agreement with previous analyses on disturbances in swirling flows, the Beltrami vorticity-induced disturbances are not purely convected by the mean flow. The disturbances, which induce a persisting static pressure field, can be shown to grow linearly in strength close to the blade-row before beginning to decay inversely with axial distance downstream. This is again in agreement with previous analyses on swirling flow in which the disturbances had their origin in the viscous blade wakes. It is further shown that this analysis only agrees with the earlier analysis, in which vorticity-induced disturbances are assumed to be purely convected by the mean flow, in the limit of large numbers of blades and in a downstream region very close to the blade row. The two analyses differ considerably further downstream; that is, this analysis can predict the downstream evolution of the three-dimensional disturbances while the earlier cannot. AFOSR Contract F49620-78-C-0084 2016-09-27T19:59:07Z 2016-09-27T19:59:07Z 1979 Technical Report http://hdl.handle.net/1721.1/104424 06606596 GT & PDL report ; no. 147 79, [45] leaves application/pdf Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1979] |
| spellingShingle | TJ778.M41 G24 no.147 Turbomachines -- Blades Compressors Vortex-motion Viscous flow Tan, Choon Sooi Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title | Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title_full | Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title_fullStr | Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title_full_unstemmed | Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title_short | Three-dimensional incompressible and compressible Beltrami flow through a highly-loaded isolated rotor |
| title_sort | three dimensional incompressible and compressible beltrami flow through a highly loaded isolated rotor |
| topic | TJ778.M41 G24 no.147 Turbomachines -- Blades Compressors Vortex-motion Viscous flow |
| url | http://hdl.handle.net/1721.1/104424 |
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