Characterization of Bending Stiffness for Honeycomb Sandwich Plate in Three-point Bending Test Using Mechanics of Structure Genome

2019 ◽  
Author(s):  
BANGHUA ZHAO ◽  
WENBIN YU ◽  
JAFFE TSENG ◽  
RONG CHIU
Keyword(s):  
Sandwich Plate ◽  
Bending Stiffness ◽  
Bending Test ◽  
Three Point Bending ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Plate

scholarly journals Lightweight Design of Solar UAV Wing Structures Based on Sandwich Equivalent Theory

2021 ◽  
Vol 2021 ◽  
pp. 1-12
Author(s):  
Hongjun Liu ◽  
Dong Zhou ◽  
Bing Shen ◽  
You Ding
Keyword(s):  
Topology Optimization ◽  
Sandwich Plate ◽  
Lightweight Design ◽  
Equivalent Model ◽  
Three Point Bending ◽  
Equivalent Theory ◽  
Actual Model ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Plate ◽  
Wing Structures

In this paper, an equivalent method based on sandwich plate is deduced, and the equivalent parameters of the honeycomb plate are obtained. With these equivalent parameters, the honeycomb plate equivalent FEM simulation model and actual model are established, and three-point bending simulations of the equivalent model and the actual model three-point are completed. Then, a three-point bending test of a real honeycomb sandwich panel was performed for comparison with the simulation result, which agrees well with the test result and shows the effectiveness of the equivalent model. The equivalent model of honeycomb sandwich plate win ribs is established for structural topology optimization and wing static simulation analysis, and a prototype of the solar UAV is made for flight testing according to the topology optimization results. The simulation and prototype test results indicated that the sandwich equivalent theory is suitable for the lightweight design of solar UAV wing structures with honeycomb sandwich plate materials, and this method can provide a reference for the same type of wing structure design.

Mechanical Property and Oxidation Behavior of LPS-SiC Materials

2006 ◽  
Vol 321-323 ◽  
pp. 913-916
Author(s):  
Sang Ll Lee ◽  
Yun Seok Shin ◽  
Jin Kyung Lee ◽  
Jong Baek Lee ◽  
Jun Young Park
Keyword(s):  
Mechanical Property ◽  
Fracture Toughness ◽  
Oxidation Behavior ◽  
Elevated Temperatures ◽  
Indentation Test ◽  
Bending Test ◽  
Secondary Phases ◽  
Three Point Bending ◽  
Different Temperatures

The microstructure and the mechanical property of liquid phase sintered (LPS) SiC materials with oxide secondary phases have been investigated. The strength variation of LPS-SiC materials exposed at the elevated temperatures has been also examined. LPS-SiC materials were sintered at the different temperatures using two types of Al2O3/Y2O3 compositional ratio. The characterization of LPS-SiC materials was investigated by means of SEM with EDS, three point bending test and indentation test. The LPS-SiC material with a density of about 3.2 Mg/m3 represented a flexural strength of about 800 MPa and a fracture toughness of about 9.0 MPa⋅√m.

scholarly journals Characterization of mortar fracture based on three point bending test and XFEM

2018 ◽  
Vol 11 (4) ◽  
pp. 339-344 ◽  
Author(s):  
Yucheng Huang ◽  
Yanhua Guan ◽  
Linbing Wang ◽  
Jian Zhou ◽  
Zhi Ge ◽  
...  
Keyword(s):  
Bending Test ◽  
Three Point Bending

Numerical Simulation of Penetration Effect of Spherical Fragment on Square Honeycomb Sandwich Plate

2011 ◽  
Vol 474-476 ◽  
pp. 1869-1873 ◽  
Author(s):  
Tao Wang ◽  
Wen Li Yu ◽  
San Qiang Dong ◽  
Yun Liang Gao
Keyword(s):  
Oblique Incidence ◽  
Sandwich Plate ◽  
Normal Incidence ◽  
Impact Angle ◽  
Damage Effect ◽  
Penetration Effect ◽  
Honeycomb Sandwich ◽  
Honeycomb Sandwich Plate ◽  
Solid Plate ◽  
Active Fragment

In this paper, a spherical fragment penetrating to square honeycomb sandwich plate and solid plate which has the same mass as sandwich plate are simulated by LS-DYNA code. The fragment impacts plates at normal incidence and oblique incidence with 30º impact angle at the velocity of 300m/s, 350m/s, 380m/s, 400m/s, 450m/s and 500m/s separately. And the damage pattern of sandwich plate, the acceleration of fragment and the energy absorption of sandwich plate are acquired. For sandwich plate, the acceleration of fragment is less than that of solid plate and the internal energy absorbed is larger that that of solid plate. The result can be used to design new active fragment to improve the damage effect to sandwich plate.

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