Buckling under the action of loading by aerodynamic and inertial forces during ground track tests of aviation equipment

The article analyses the choice of a rational layout of the test object with a propulsion system (PS). One of the design examples of calculating the longitudinal stability and strength of the structure is given. The purpose of the article is to solve the problem of bending the elastic line of a cant...

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Bibliographic Details
Main Authors: Sergey A. ASTAKHOV, Vasiliy I. BIRYUKOV
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2021-08-01
Series:INCAS Bulletin
Subjects:
Online Access:https://bulletin.incas.ro/files/astakhov_biryukov_vol_13_special_issue.pdf