scholarly journals Mechanical modeling of bending stiffness degradation for soft-honeycomb sandwich structure under CW laser heating

AIP Advances ◽  
2020 ◽  
Vol 10 (2) ◽  
pp. 025201 ◽  
Author(s):  
Jiawei Wang ◽  
Bin Li ◽  
Yongxiang Zhu ◽  
Weiping Liu ◽  
Lixiong Wu ◽  
...  
Keyword(s):  
Laser Heating ◽  
Sandwich Structure ◽  
Bending Stiffness ◽  
Stiffness Degradation ◽  
Mechanical Modeling ◽  
Cw Laser ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Structure

High-Frequency Vibration Response of Metal Honeycomb Sandwich Structure

2009 ◽  
Vol 79-82 ◽  
pp. 1727-1730 ◽  
Author(s):  
Xiao Dong He ◽  
Xiang Hao Kong ◽  
Li Ping Shi ◽  
Ming Wei Li
Keyword(s):  
High Frequency ◽  
Sandwich Structure ◽  
Dynamic Pressure ◽  
Vibration Response ◽  
Element Analysis ◽  
High Frequency Vibration ◽  
Honeycomb Sandwich ◽  
Vibration Experiment ◽  
Aerial Vehicle ◽  
Honeycomb Sandwich Structure

ARMOR TPS panel is above the whole ARMOR TPS, and the metal honeycomb sandwich structure is the surface of the ARMOR TPS panel. So the metal honeycomb sandwich structure plays an important role in the ARMOR TPS, while it bears the flight dynamic pressure and stands against the flight dynamic calefaction. So the active environment of metal honeycomb sandwich structure is very formidable. We have to discuss any extreme situation, for reason of making sure aerial vehicle is safe. And high-frequency vibration is one of active environment. In this paper we have analyzed high-frequency vibration response of metal honeycomb sandwich structure. We processed high-frequency vibration experiment by simulating true aerial environment. Sequentially we operated high-frequency vibration experiment of metal honeycomb sandwich structure with cracks, notches and holes. Then finite-element analysis was performed by way of validating the experiment results. Haynes214 is a good high temperature alloy material of both face sheet and core at present, so we choose it in this paper.

Honeycomb-Cored Sandwich Structure Composites

2010 ◽  
pp. 223-235
Keyword(s):  
Composite Materials ◽  
Sandwich Structure ◽  
Complex Structure ◽  
Failure Mechanisms ◽  
Resin System ◽  
Lower Weight ◽  
Film Adhesive ◽  
Adhesive Prepreg ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Structure

Abstract The honeycomb sandwich structure composite is a very efficient and complex structure widely used in the aircraft industry. Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This chapter describes the analysis of the intermingling of the film adhesive/prepreg resin system. It discusses the causes and effects of honeycomb core movement, which results in core crush. The chapter also explains the formation of a void in honeycomb composites and the failure mechanisms in honeycomb sandwich structure composites.

Failure study of honeycomb sandwich structure with embedded part under axial pullout loading

2020 ◽  
Vol 146 ◽  
pp. 106489 ◽  
Author(s):  
Ruixiang Bai ◽  
Hongqi Ou ◽  
Kewang Peng ◽  
Wen Wu ◽  
Zhenkun Lei ◽  
...  
Keyword(s):  
Sandwich Structure ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Structure

Bending properties of three-dimensional honeycomb sandwich structure composites: experiment and Finite Element Method simulation

2017 ◽  
Vol 88 (17) ◽  
pp. 2024-2031 ◽  
Author(s):  
Lihua Lv ◽  
Yaoli Huang ◽  
Jingrui Cui ◽  
Yongfang Qian ◽  
Fang Ye ◽  
...  
Keyword(s):  
Failure Mode ◽  
Cross Section ◽  
Sandwich Structure ◽  
Three Dimensional ◽  
Finite Element Method Simulation ◽  
Cross Section Shape ◽  
Section Shape ◽  
Honeycomb Sandwich ◽  
Bending Failure ◽  
Honeycomb Sandwich Structure

This paper fabricated three-dimensional (3D) honeycomb sandwich structure fabrics with three different cross-section shapes on an ordinary loom by reasonable design with low cost. The 3D honeycomb sandwich structure composites were fabricated by the vacuum assisted resin transfer molding process. Then, the bending properties of 3D honeycomb sandwich structure composites with different cross-section shapes were tested. The results showed that the 3D honeycomb sandwich structure composite with a hexagonal cross-section shape had the maximum load, the 3D honeycomb sandwich structure composite with a triquetrous cross-section shape had the minimum load and the 3D honeycomb sandwich structure composite with a quadrangular cross-section shape had a load between the two. The bending failure mode showed that the 3D honeycomb sandwich structure composite had a typical bending failure mode with compression failure in the front and tensile failure in the back. Finally, the load–displacement curves and failure mode were obtained by FEM (Finite Element Method) simulation with ABAQUS software. The good agreements of comparisons proved the validity of the FEM.

Sign in / Sign up

Export Citation Format

Share Document