z-logo
open-access-imgOpen Access
Experience of computational research on the flutter of an unmanned aerial vehicle
Author(s) -
Valeriy Arkadievich Mosunov,
Р. В. Рябыкина,
В. И. Смыслов,
А. В. Фролов
Publication year - 2018
Publication title -
vestnik koncerna vko «almaz - antej»
Language(s) - English
Resource type - Journals
ISSN - 2542-0542
DOI - 10.38013/2542-0542-2018-2-18-25
Subject(s) - flutter , aerodynamics , aeroelasticity , parametric statistics , antisymmetric relation , aerospace engineering , set (abstract data type) , computer science , software , structural engineering , engineering , mathematics , statistics , mathematical physics , programming language
The paper focuses on the sequence of computational and experimental investigations on the flutter. We set the initial data for the unmanned aerial vehicle and built the mathematical models. Furthermore, we did parametric analysis of symmetric and antisymmetric flutter shapes of the wings and the tail, studied the aerodynamics effect on the body of the vehicle, gave the examples of the calculation data on the base of KS-M and MSC. Nastran software.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here