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| Authors: Lashko V.A., Passar A.V. | Published: 21.03.2014 |
| Published in issue: #2(593)/2008 | |
| Category: Transportation and Power Engineering | |
| Keywords: |
In work problems of a choice of geometrical parameters of a flowing part of the radially-axial turbine are stated at designing. For the analysis of the chosen geometrical parameters it is offered to use JA.A. Sirotkin s mathematical model of a direct problem of an axisymmetric eddy flow. Results of calculations on an example of the radially-axial turbine of turbo-compressor TKR-14V-30 are resulted.