Asymmetric inlet flow in axial turbomachines
May 1959
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| Format: | Technical Report |
| Published: |
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1959
2016
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| Online Access: | http://hdl.handle.net/1721.1/104671 |
| _version_ | 1811094867135168512 |
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| author | Seidel, Barry S. (Barry Stanley) |
| author2 | Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine Laboratory Seidel, Barry S. (Barry Stanley) |
| author_sort | Seidel, Barry S. (Barry Stanley) |
| collection | MIT |
| description | May 1959 |
| first_indexed | 2024-09-23T16:06:46Z |
| format | Technical Report |
| id | mit-1721.1/104671 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T16:06:46Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1959 |
| record_format | dspace |
| spelling | mit-1721.1/1046712019-04-12T16:17:53Z Asymmetric inlet flow in axial turbomachines Seidel, Barry S. (Barry Stanley) Massachusetts Institute of Technology. Gas Turbine Laboratory TJ267.A1 M37 no.51 Turbomachines -- Fluid dynamics Rotors May 1959 Includes bibliographical references (leaves 53-55) A modified actuator disc analysis is made which, through an improved prediction of the blade forces, attempts to give closer correspondence with experiment than the previous theory. The fluid is assumed inviscid and incompressible. Perturbations to the two-dimensional flow through an isolated blade row are considered. The steady flow equations of motion and continuity are linearized. According to experiments conducted on an isolated compressor rotor, the present theory offers an improvement, compared to previous theory, in the prediction of distortion attenuation, effects of flow rate, and effects of varying chord/spacing ratio. Under the Sponsorship of: General Electric Company, Westinghouse Electric Corporation and Allison Division of General Motors Corporation 2016-10-06T21:21:51Z 2016-10-06T21:21:51Z 1959 Technical Report http://hdl.handle.net/1721.1/104671 09162313 GTL report #51 55, [46] leaves application/pdf Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1959 |
| spellingShingle | TJ267.A1 M37 no.51 Turbomachines -- Fluid dynamics Rotors Seidel, Barry S. (Barry Stanley) Asymmetric inlet flow in axial turbomachines |
| title | Asymmetric inlet flow in axial turbomachines |
| title_full | Asymmetric inlet flow in axial turbomachines |
| title_fullStr | Asymmetric inlet flow in axial turbomachines |
| title_full_unstemmed | Asymmetric inlet flow in axial turbomachines |
| title_short | Asymmetric inlet flow in axial turbomachines |
| title_sort | asymmetric inlet flow in axial turbomachines |
| topic | TJ267.A1 M37 no.51 Turbomachines -- Fluid dynamics Rotors |
| url | http://hdl.handle.net/1721.1/104671 |
| work_keys_str_mv | AT seidelbarrysbarrystanley asymmetricinletflowinaxialturbomachines |