Determination of Mechanical Properties of Composites Based on the Static Test Results

The paper considers the results of the static test of the wing-to-body juncture spar of the composite unmanned aerial vehicle. The beam-cantilever anchoring model is used. To determine the mechanical characteristics of the material, a technique based on the response of the structure to the lateral l...

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Bibliographic Details
Published in:Russian aeronautics 2023-12, Vol.66 (4), p.910-915
Main Authors: Kostin, V. A., Garaev, A. M.
Format: Article
Language:English
Subjects:
Automotive Engineering
Cantilever beams
Engineering
Lateral loads
Mechanical properties
Static tests
Structural Mechanics and Strength of Flight Vehicles
Unmanned aerial vehicles
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Summary:The paper considers the results of the static test of the wing-to-body juncture spar of the composite unmanned aerial vehicle. The beam-cantilever anchoring model is used. To determine the mechanical characteristics of the material, a technique based on the response of the structure to the lateral load is used.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799823040335