Simulation of an aerodynamic profile with sections of ad hoc concavity

The article describes the study carried out by the authors of the use of parametric geometric models to reduce the complexity of the design of parts that follow the theoretical contour of the bearing surfaces of the aircraft. Also, an algorithm that allows eliminating the existing ad hoc concavity p...

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Bibliographic Details
Main Authors: Pocebneva Irina, Deniskin Yuri, Yerokhin Alexandr, Artiukh Viktor, Vershinin Vladimir
Format: Article
Language:English
Published: EDP Sciences 2019-01-01
Series:E3S Web of Conferences
Online Access:https://www.e3s-conferences.org/articles/e3sconf/pdf/2019/36/e3sconf_spbwosce2019_01074.pdf
Description
Summary:The article describes the study carried out by the authors of the use of parametric geometric models to reduce the complexity of the design of parts that follow the theoretical contour of the bearing surfaces of the aircraft. Also, an algorithm that allows eliminating the existing ad hoc concavity profile is considered.
ISSN:2267-1242