Open AccessExperimental and numerical determination of the bearing capacity of the honeycomb panel with potted inserts when loading the panel in its plane
Author(s) -
С. Н. Перов,
S.V. Glushkov,
Dmitriy Stepanets
Publication year - 2019
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/666/1/012021
Subject(s) - honeycomb , spacecraft , structural engineering , frame (networking) , bearing capacity , plane (geometry) , flat panel , power (physics) , engineering , materials science , computer science , mechanical engineering , composite material , physics , aerospace engineering , mathematics , geometry , computer graphics (images) , quantum mechanics
A typical three-layer honeycomb panel of a spacecraft (SC) is considered. For connection to the power frame of the spacecraft, as well as for rigging works, embedded elements (inserts) are installed in the panel. The results of experimental and numerical determination of the bearing capacity of the panel in the places of installation of potted inserts under the action of the load in its plane are presented in the article.