赵冉, 宋巧治, 陈浩宇, et al. Analysis and Verification of Self-weight Influence on Large Deformation of Highly Flexible Cantilever Beams[J]. Mechanical Science and Technology for Aerospace Engineering, 2026, 45(2): 345-350.
DOI:
赵冉, 宋巧治, 陈浩宇, et al. Analysis and Verification of Self-weight Influence on Large Deformation of Highly Flexible Cantilever Beams[J]. Mechanical Science and Technology for Aerospace Engineering, 2026, 45(2): 345-350. DOI: 10.13433/j.cnki.1003-8728.20250111.
Analysis and Verification of Self-weight Influence on Large Deformation of Highly Flexible Cantilever Beams
The highly flexible cantilever beam can undergo obvious initial deformation due to gravity
which in turn affects the geometric stiffness of the beam and jointly dominates the large deformation response of the structure under the combined action of other external loads. To determine the influence of the self-weight on static large deformation characteristics
the theoretical model of cantilever beams is given considering self-weight and tip load
and the numerical simulation model of highly flexible beams is established based on the nonlinear finite element method. The self-weight of the beam is regarded as a uniformly distributed load with constant direction
and the large deformation behaviors under different self-weights are analyzed. On this basis
a large deformation static experiment with or without gravity effect is carried out for a highly flexible beam model
and the numerical simulation results are compared with the experimental results
and the error is within the allowable range of the engineering. The comprehensive finite element analysis and experimental research results show that the influence of the initial deformation caused by gravity on the large deformation of highly flexible beam under external loads cannot be ignored
and it should be fully considered in engineering design
the finite element simulation results of large deformation considering gravity have satisfactory accuracy and can be used for practical engineering analysis.