Modelling, structural optimization and transient thermal analysis of honeycomb structure

• Published in: AIP conference proceedings Vol. 2937; no. 1
• Main Authors: Kumar, Edagapur Kiran, Krishna Palla, Satya, Prabu, D. Antony
• Format: Journal Article Conference Proceeding
• Language: English
• Published: Melville American Institute of Physics 02.08.2024
• Subjects: Honeycomb structures; Material properties; Modal analysis; Stress analysis; Thermal analysis; Thickness
• ISSN: 0094-243X; 1551-7616
• DOI: 10.1063/5.0219440

Honeycomb structures of various thicknesses and introductions are the subject of this investigation. The primary goal is to create a fabric demonstration that is comparable in thickness to the fabric with a strong thickness. In light of the limited component investigations, significant preferences can be gained in terms of ease of displaying and demonstrating adjustment, arrangement time, and equipment assets by substituting the recently planned show for the strong solid strong thickness structure. A comparison is made to identify the best possible model from the suppositions of expository models that can be found in the writing. First, the sandwich pillars with four distinct honeycomb centres are shown in detail, and these models are acknowledged as a starting point. Proportionate models with the same measurements are created at this point. A variety of thoughts are used to determine the material properties of the corresponding models in the writing. As a result, it is recommended that the equivalent model be used for stress analysis during the initial design phase. Deflection, modal analysis, stiffness determination, and deformations can all be performed with confidence using the newly developed model. In this project, the distance between each honeycomb is 75mm, with a total of 10 units along each of the two axes.