Show simple item record

contributor authorJiang, Shi
contributor authorGuo-Ping, Cai
date accessioned2023-08-16T18:12:19Z
date available2023-08-16T18:12:19Z
date copyright3/20/2023 12:00:00 AM
date issued2023
identifier issn1555-1415
identifier othercnd_018_05_051003.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291613
description abstractThis paper proposes a extend linear equivalent method that can extend the linear equivalent micropolar beam model to the nonlinear equivalent micropolar beam model to analyze nonlinear vibration for large space truss structure, and also proposes a lattice enhancement method to improve the cantilever truss for the buckling problem that exists in space cantilever truss structures. The nonlinear equivalent model is obtained by introducing a corotating coordinate system into the linear equivalent beam model. Since the instability of the fixed root end of the cantilever truss is the main reason for buckling, the method of strengthening the longeron of the truss lattice by lattice is proposed. The accuracy of the equivalent geometric nonlinear model and the effectiveness of the improved cantilever truss structure are verified by four numerical simulation examples. The methods proposed in this paper provide some reference for studying the dynamics analysis of large space trusses and the design of structures.
publisherThe American Society of Mechanical Engineers (ASME)
titleEquivalent Beam Model and Improved Structure Design of Large Space Antenna Truss With Geometric Nonlinearity
typeJournal Paper
journal volume18
journal issue5
journal titleJournal of Computational and Nonlinear Dynamics
identifier doi10.1115/1.4057043
journal fristpage51003-1
journal lastpage51003-11
page11
treeJournal of Computational and Nonlinear Dynamics:;2023:;volume( 018 ):;issue: 005
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record