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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2024
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Article
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Tab 6
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Research Article
Research on the Simulation Method for Equivalent Stiffness of Bolted Connection Thin Plate Structures
Table 6
Parameter identification results for the bolted beam structure in various operating conditions.
Stimulation force 10 N
Stimulation force 12.5 N
Stimulation force 15 N
Bolt preload 1 KN
Bolt preload 2.5 KN
Bolt preload 5 KN
Bolt preload 10 KN