Study on effect of some geometric transformations of the trailing edge of airfoils on their aerodynamic parameters
The work objective is to evaluate how the geometric transformations of the trailing edge of some airfoils affect the aerodynamic characteristics. Such transformations as the trailing edge thickening and rounding are considered. The performance of Wortmann FX 63-137, NACA 23024 и Clark Y is calculate...
Main Authors: | , |
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Format: | Article |
Language: | Russian |
Published: |
Don State Technical University
2016-09-01
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Series: | Advanced Engineering Research |
Subjects: | |
Online Access: | https://www.vestnik-donstu.ru/jour/article/view/93 |