Linear and nonlinear free vibration analysis of super-light composite beams with honeycomb core layer and adjustable Poisson’s ratio using multiple-scale method

Eipakchi, Hamidreza; Nasrekani, Farid Mahboubi

doi:10.1007/s00707-022-03354-9

Cited by 6 publications

(2 citation statements)

References 33 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Aghazadeh et al [188] implemented various beam methodologies for investigating the FV and static analysis of NMS FG beams. However, by using a multiple-scale methodology, Eipakchi and Nasrekani [189] investigated the linear/NL FV analysis of extreme-light composite beams, including a honeycomb core. Likewise, Ke et al [190] examined the NL FV behavior of FG-CNT-reinforced composite beam structures.…”

Section: Beam Structurementioning

confidence: 99%

Computational Linear and Nonlinear Free Vibration Analyses of Micro/Nanoscale Composite Plate-Type Structures With/Without Considering Size Dependency Effect: A Comprehensive Review

Al Mahmoud,

Safaei,

Sahmani

et al. 2024

Arch Computat Methods Eng

View full text Add to dashboard Cite

Recently, the mechanical performance of various mechanical, electrical, and civil structures, including static and dynamic analysis, has been widely studied. Due to the neuroma's advanced technology in various engineering fields and applications, developing small-size structures has become highly demanded for several structural geometries. One of the most important is the nano/micro-plate structure. However, the essential nature of highly lightweight material with extraordinary mechanical, electrical, physical, and material characterizations makes researchers more interested in developing composite/laminated-composite-plate structures. To comprehend the dynamical behavior, precisely the linear/nonlinear-free vibrational responses, and to represent the enhancement of several parameters such as nonlocal, geometry, boundary condition parameters, etc., on the free vibrational performance at nano/micro scale size, it is revealed that to employ all various parameters into various mathematical equations and to solve the defined governing equations by analytical, numerical, high order, and mixed solutions. Thus, the presented literature review is considered the first work focused on investigating the linear/nonlinear free vibrational behavior of plates on a small scale and the impact of various parameters on both dimensional/dimensionless natural/fundamental frequency and Eigen-value. The literature is classified based on solution type and with/without considering the size dependency effect. As a key finding, most research in the literature implemented analytical or numerical solutions. The drawback of classical plate theory can be overcome by utilizing and developing the elasticity theories. The nonlocality, weight fraction of porosity, or the reinforcements, and its distribution type of elastic foundation significantly influence the frequencies.

show abstract

Section: Beam Structurementioning

confidence: 99%

Computational Linear and Nonlinear Free Vibration Analyses of Micro/Nanoscale Composite Plate-Type Structures With/Without Considering Size Dependency Effect: A Comprehensive Review

Al Mahmoud,

Safaei,

Sahmani

et al. 2024

Arch Computat Methods Eng

View full text Add to dashboard Cite

show abstract

“…Due to the diverse components and intricate internal structure inherent in honeycomb sandwich panels, ensuring accurate model predictions necessitates extensive calculations. This poses a challenge to the performance and memory requirements of the computers, which, in turn, affects computing efficiency [21,22]. Therefore, further experiments and further studies are needed to obtain an accurate model for the damping properties of all kinds of honeycomb sandwich panels.…”

Section: Introductionmentioning

confidence: 99%

Research on Dynamic Response under the External Impact of Paper Honeycomb Sandwich Board

Lin,

Hu,

et al. 2024

Materials

View full text Add to dashboard Cite

The dynamic mechanical behavior and cushioning performance of honeycomb sandwich panels, which are extensively employed in product cushioning packaging due to their exceptional energy absorption capabilities, were examined using a combination of experimental and numerical methods. Several factors, such as maximum acceleration–static stress, cushioning coefficient–static stress, and other curves, were analyzed under various impact conditions. The simulated stress–strain, deformation modes, cushioning coefficients, and other parameters demonstrate consistency with the experimental results. The acceleration, maximum compression, and cushioning coefficient obtained from the experiment and simulation calculation were 30.68 g, 15.44 mm, and 2.65, and 31.96 g, 14.91 mm, and 2.79, respectively. The results indicate that all error values were less than 5%, confirming the precision and reliability of the model. Furthermore, the model was utilized to simulate and predict the cushioning performance of honeycomb sandwich panels with different cell structures and paper thicknesses. These results provide a solid basis for enhancing the design of subsequent honeycomb element structures.

show abstract

Geometric nonlinear vibration theory of the Vierendeel Sandwich Plate based on generalized variational method

Liu,

Kuang,

et al. 2024

Arch Appl Mech

View full text Add to dashboard Cite

Linear and nonlinear free vibration analysis of super-light composite beams with honeycomb core layer and adjustable Poisson’s ratio using multiple-scale method

Cited by 6 publications

References 33 publications

Computational Linear and Nonlinear Free Vibration Analyses of Micro/Nanoscale Composite Plate-Type Structures With/Without Considering Size Dependency Effect: A Comprehensive Review

Computational Linear and Nonlinear Free Vibration Analyses of Micro/Nanoscale Composite Plate-Type Structures With/Without Considering Size Dependency Effect: A Comprehensive Review

Research on Dynamic Response under the External Impact of Paper Honeycomb Sandwich Board

Geometric nonlinear vibration theory of the Vierendeel Sandwich Plate based on generalized variational method

Contact Info

Product

Resources

About