Development of a method for geometrical modeling of the airfoil profile of an axial turbomachine blade
A method for geometric modeling of the contours of the suction and the pressure side profiles of axial turbomachine blades described by compound curves and formed by two sections has been proposed. Each section of the profile contour was modeled by a curve described in a natural parameterization. Th...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
PC Technology Center
2019-10-01
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| Series: | Eastern-European Journal of Enterprise Technologies |
| Subjects: | |
| Online Access: | http://journals.uran.ua/eejet/article/view/180915 |