The display of multi-dimensional flows in turbomachinery
August 1972
| Main Authors: | , |
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| Format: | Technical Report |
| Published: |
Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1972]
2016
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| Online Access: | http://hdl.handle.net/1721.1/104695 |
| _version_ | 1811086820651302912 |
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| author | Probst, Harris Carey Oliver, David A. (David Anthony), 1939- |
| author2 | Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine Laboratory Probst, Harris Carey Oliver, David A. (David Anthony), 1939- |
| author_sort | Probst, Harris Carey |
| collection | MIT |
| description | August 1972 |
| first_indexed | 2024-09-23T13:35:12Z |
| format | Technical Report |
| id | mit-1721.1/104695 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T13:35:12Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1972] |
| record_format | dspace |
| spelling | mit-1721.1/1046952019-04-12T16:17:53Z The display of multi-dimensional flows in turbomachinery Probst, Harris Carey Oliver, David A. (David Anthony), 1939- Massachusetts Institute of Technology. Gas Turbine Laboratory TJ778.M41 G24 no.111 Turbomachines -- Data processing Multiphase flow August 1972 Introduction: As part of a general development of computational techniques for multidimensional flows through turbomachine passages and over turbomachine blading at the M.I.T. Gas Turbine Laboratory, display techniques and programs have been developed for the visualization and interpretation of the computed flows. These display programs have been developed for the Adage AGT-30 system implemented at the Electronic Systems Laboratory at M.I.T. In the present report two major programs are described and illustrated. These are programs for the display of the turbomachine blading and flow passage geometry and for the display of contours of any scalar fluid variable in the flow passage. The manner in which the system is used is as follows. The turbomachine blading and flow passage geometrical data exist on an Adage tape. The output of the fluid dynamic calculation which is presently done on the OS/370 system is connected on OS/370 to an Adage compatible tape. This tape which represents the computed flow is then viewed on the Adage system. This research carried out in the Gas Turbine Laboratory, M.I.T., supported by the NASA Lewis Research Center under Grant NGL 22-009-383 2016-10-06T21:22:01Z 2016-10-06T21:22:01Z 1972 Technical Report http://hdl.handle.net/1721.1/104695 09913209 GTL report #111 18 leaves application/pdf Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1972] |
| spellingShingle | TJ778.M41 G24 no.111 Turbomachines -- Data processing Multiphase flow Probst, Harris Carey Oliver, David A. (David Anthony), 1939- The display of multi-dimensional flows in turbomachinery |
| title | The display of multi-dimensional flows in turbomachinery |
| title_full | The display of multi-dimensional flows in turbomachinery |
| title_fullStr | The display of multi-dimensional flows in turbomachinery |
| title_full_unstemmed | The display of multi-dimensional flows in turbomachinery |
| title_short | The display of multi-dimensional flows in turbomachinery |
| title_sort | display of multi dimensional flows in turbomachinery |
| topic | TJ778.M41 G24 no.111 Turbomachines -- Data processing Multiphase flow |
| url | http://hdl.handle.net/1721.1/104695 |
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