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Analysis and parametric optimization of a novel sandwich panel with double-V auxetic structure core under air blast loading

International Journal of Mechanical Sciences, 2018
Blast shock wave is a big threat to the military vehicle and may cause vehicle damages and passenger casualties. It is a big issue to balance the protective performance and lightweight property of military vehicle.
Yuanlong Wang   +3 more
semanticscholar   +1 more source

Mechanical response of a novel composite Y-frame core sandwich panel under shear loading

Composite structures, 2019
The hot-press molding method was developed to fabricate a novel composite Y-frame core sandwich panel in this paper. The shear experiments were conducted to investigate the shear mechanical response of the composite Y-frame core sandwich panels with ...
Jialin Liu   +3 more
semanticscholar   +1 more source

Sound transmission loss of sandwich panel with closed octahedral core

Journal of Sandwich Structures and Materials, 2019
In this paper, an ultralightweight sandwich panel with closed octahedral core is proposed, which demonstrates excellent acoustic property of sound transmission loss as well as great mechanical performance.
Zhi-Hui Wen, Dong-wei Wang, Li Ma
semanticscholar   +1 more source

Sandwich panel repair

1997
This chapter will briefly go over some of the types of damage that honeycomb sandwich panels suffer and the principles of repair. Military Handbook 337 (1982) Adhesive Bonded Aerospace Structural Repair is an excellent source for detailed repair procedures. It replaces and updates the old Military Handbook 23 (1968) repair section.
openaire   +1 more source

Mechanical behaviors of C/SiC pyramidal lattice core sandwich panel under in-plane compression

Composite structures, 2019
C/SiC composite lattice-core sandwich panels combined with thermal insulation and load-bearing capacities are considered as the most promising candidates for thermal protection system (TPS). In this study, C/SiC pyramidal lattice-core sandwich panel with
Yanfei Chen   +6 more
semanticscholar   +1 more source

Theoretical deflection analysis of multi-walled carbon nanotube reinforced sandwich panel and experimental verification

Composites Part B: Engineering, 2019
In this article, the influence of the multi-walled carbon nanotube reinforcement on the stiffness of sandwich curved panel is examined theoretically via deflection analysis and compared with own experimental data for the verification of accuracy.
K. Mehar, S. Panda
semanticscholar   +1 more source

Structural-Acoustic Optimization of Sandwich Panels

Journal of Vibration and Acoustics, 2005
Sandwich panels comprising face sheets enclosing a core are increasingly common structural elements in a variety of applications, including aircraft fuselages, flight surfaces, vehicle panels, lightweight enclosures, and bulkheads. This paper presents the optimization of various innovative sandwich configurations for minimization of their structural ...
FRANCO, FRANCESCO   +2 more
openaire   +4 more sources

Response of Chiral Auxetic Composite Sandwich Panel to Fragment Simulating Projectile Impact

physica status solidi (b), 2019
The chiral auxetic cellular structures are fabricated using SEBM (selective electron beam melting) method and tested under compressive loading. The results of experimental testing are used for validation of the computational model in LS‐DYNA. Furthermore,
N. Novak   +4 more
semanticscholar   +1 more source

Drop weight impact tests on composite sandwich panel of aluminum foam and epoxy resin

Mechanics of Advanced Materials and Structures, 2019
The composite sandwich panel of aluminum foam and epoxy resin uses epoxy resin and aluminum foam interpenetration to form a composite surface layer, which makes the surface layer and core material a whole and greatly improves the integrity of the ...
Ya‐jun Xin   +3 more
semanticscholar   +1 more source

Nonlinear Dynamic Buckling of Sandwich Panels

Journal of Applied Mechanics, 1976
Nonlinear dynamic buckling of simply supported rectangular sandwich panels with isotropic cores and with initial curvature under transverse loads is analyzed. The large deflection sandwich panel equations proposed by Reissner are solved using a trigonometric series spacewise and by Houbolt scheme for timewise integration.
Murthy, N. K. Adi, Alwar, R. S.
openaire   +2 more sources

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