Mechanical modeling of bending stiffness degradation for soft-honeycomb sandwich structure under CW laser heating
Source abstract
Abstract
Based on the theory of Reissner’s sandwich structure bending, a mechanical model of bending stiffness degradation for a soft-honeycomb sandwich structure under continuous wave (CW) laser heating was established by introducing the equivalent debonding coefficient of adhesive and elastic modulus temperature dependence of panels. To verify the rationality of the mechanical model, a real-time bending stiffness measurement system for a soft-honeycomb sandwich structure under CW laser heating was proposed using the overhanging beam three-point bending method. The results show that the mechanical model works good to describe the decreasing trend of the soft-honeycomb sandwich structure under CW laser heating and to predict the residual bending stiffness after CW laser heating, despite the fact that in the early stage of CW laser heating, the bending stiffness of some kind of soft-honeycomb sandwich structure may increase for a short time due to the pyrolysis gas production. However, with the overflowing of pyrolysis gas and the elastic modulus of panel degradation at a high temperature, the bending stiffness of soft-honeycomb sandwich structure declines rapidly and soon fails to withstand any bending load. The research shows that special attention should be paid to the effect of laser heating on the mechanical properties of the soft-honeycomb sandwich structure. It also enlightens the study of mechanical properties and temperature dependence of the honeycomb sandwich structure at a high heating rate.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Laser and Thermal Forming Techniques · Structural Analysis of Composite Materials · Engineering Applied Research
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
State Key Laboratory of Laser Interaction with Matter, Northwest Institute of Nuclear Technology 1 , Xi’an 710024, China
College of Aeronautics, Northwestern Polytechnical University 2 , Xi’an 710072, China
Funding
State Key Laboratory of Laser Interaction with Matter [China]
References (29)
Show source-provided references
1. Testing and modeling of NomexTM honeycomb sandwich Panels with bolt insert10.1016/j.compositesb.2013.09.006 ↗
2. Modelling of low-energy/low-velocity impact on Nomex honeycomb sandwich structures with metallic skins10.1016/j.ijimpeng.2007.02.008 ↗
3. Compression after impact test (CAI) on NOMEXTM honeycomb sandwich panels with thin aluminum skins10.1016/j.compositesb.2014.07.015 ↗
4. A study on composite honeycomb sandwich panel structure10.1016/j.matdes.2007.03.003 ↗
5. Mechanical response of metallic honeycomb sandwich panel structures to high-intensity dynamic loading10.1016/j.ijimpeng.2007.06.008 ↗
6. Flexural creep behavior of sandwich panels containing Kraft paper honeycomb core and wood composite skins10.1016/j.msea.2011.03.092 ↗
7. Three-point bending of honeycomb sandwich beams with facesheet perforations10.1007/s10409-017-0734-z ↗
8. Investigation of mechanical properties of sandwich panels made of paper honeycomb core and wood composite skins by experimental testing and finite element (FE) modeling methods10.1007/s00107-014-0782-z ↗
9. Collapse modes in aluminium honeycomb sandwich panels under bending and impact loading10.1016/j.ijimpeng.2011.12.002 ↗
10. Experimental and numerical characterization of honeycomb sandwich composite panels10.1016/j.simpat.2009.05.008 ↗
11. Damage characterization of three point bended honeycomb sandwich structures under different temperatures with cone beam computed tomography technique10.1002/pc.23900 ↗
12. Mechanical properties analysis on honeycomb sandwich structure considering flexural rigidity of face sheets
13. Interfacial mechanical performance of composite honeycomb sandwich panels for aerospace applications10.1007/s13369-016-2307-z ↗
14. Experimental study on the temperature effect on the flexural properties of Nomex honeycomb sandwich structure10.3788/m0001820164501.120004 ↗
15. Effect of temperature and hybridisation on the low velocity impact behavior of hemp-basalt/epoxy composites10.1016/j.compstruct.2015.01.037 ↗
16. Laser cutting of carbon fiber reinforced plastics-investigation of hazardous process emissions10.1016/j.phpro.2014.08.030 ↗
17. Calibrated heat flow model for the determination of different heat-affected zones in single-pass laser-cut CFRP using a CW CO2 laser10.1007/s00339-014-8932-z ↗
18. Experimental study on the CO2 laser cutting of carbon fiber reinforced plastic composite10.1016/j.compositesa.2012.02.012 ↗
19. Estimation of the heat-affected zone in carbon fiber reinforced plastics exposed to CW radiation of the ytterbium fiber laser10.3103/s1068335619020088 ↗
20. Degradation of shear stiffness of Nomex honeycomb sandwich panel in laser irradiation
21. Finite deflections of sandwich plates10.2514/8.11610 ↗
22. Flexure analysis of unsymmetric orthotropic beams with an interlayer10.1016/j.ijsolstr.2008.07.024 ↗
23. Advances in the structural modeling of elastic sandwich panels10.1080/15376490490451561 ↗
24. Large deflection analysis of rhombic sandwich plates placed on elastic foundation
25. Mechanical modeling on the bending stiffness temperature dependence of Nomex honeycomb sandwich structure
26. Bending stiffness of inflatable tubes with external constraints
27. Dynamic testing and analysis of inflatable beams10.4028/www.scientific.net/amm.226-228.546 ↗
28. Wrinkling prediction of cylindrical and conical inflated cantilever beams under torsion and bending10.1016/j.tws.2006.01.003 ↗
29. Bending and buckling of inflatable beams: Some new theoretical results10.1016/j.tws.2005.03.005 ↗