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...

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Bibliographic Details
Main Authors: Konstantin I. Mescheryakov, Mezhlum A. Sumbatyan
Format: Article
Language:Russian
Published: Don State Technical University 2016-09-01
Series:Advanced Engineering Research
Subjects:
Online Access:https://www.vestnik-donstu.ru/jour/article/view/93