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Dynamic modeling of honeycomb sandwich panel
Archive of Applied Mechanics, 2007zbMATH Open Web Interface contents unavailable due to conflicting licenses.
GUJ L, SESTIERI, Aldo
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Modal density of sandwich panels based on an improved ordinary sandwich panel theory
Composite Structures, 2015Abstract Modal density of sandwich panels with composite face sheets and orthotropic core is presented based on an improved ordinary sandwich panel theory. The governing equations are derived by applying the Hamilton’s principle, where in-plane rigidity of the core is considered and the material and reference axes are not limited to be identical to ...
Jingyong Han +3 more
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Experimental and analytical investigation of sandwich panels
1999In order to optimize outer walls thickness and to reduce the required construction phases (costs) carrying walls built as sandwich panels (insulated wall panels) seem to be a reasonable alternative. Finished wall consists of inside insulation and two concrete wythes connected by shear connectors. It acts as composite wall up to a certain point. Load
Sigmund, Vladimir +2 more
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Nonlinear Dynamic Buckling of Sandwich Panels
Journal of Applied Mechanics, 1976Nonlinear 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.
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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.
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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.
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Response of stiffened sandwich panels
22nd Structures, Structural Dynamics and Materials Conference, 1981An increasingly important part of the design of skin-stringer systems, such as those found in flight vehicles, is the ability to reduce surface vibration levels when they are subjected to the dynamic loads of jet, or propeller noise. One common method of reducing the response of these structures is by layered construction using viscoelastic materials ...
M. SLAZAK, R. VAICAITIS
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X-joints in Composite Sandwich Panels
1998The small structural weight of fast large ships such as fast mono hulls or catamaran type of ships is of extreme importance to their success. One possible light weight structural solution is the sandwich panel with fibre reinforced laminates and a balsa, honeycomb or foam core.
Vredeveldt, A.W., Janssen, G.Th.M.
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2014
To increase insight in the behaviour of non-reinforced sandwich panels with openings, experiments, finite element simulations and analytical models have been developed and compared. Analytical models have been developed to determine the global deformations of sandwich panels without cracks.
Jorissen, A.J.M. +3 more
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To increase insight in the behaviour of non-reinforced sandwich panels with openings, experiments, finite element simulations and analytical models have been developed and compared. Analytical models have been developed to determine the global deformations of sandwich panels without cracks.
Jorissen, A.J.M. +3 more
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Wood-strand sandwich panels for panelized construction
2015Academic Journal of Civil Engineering, Vol 33 No 2 (2015): Special Issue - ICBBM ...
White, N., Voth, C., Yadama, V.
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2012
The localized wrinkling instability, and the overall buckling of these panels due to axial compression and shear loading are presented. Numerically the finite strip method, the finite prism method, and the finite layer method are especially efficient in analyzing prismatic members such as these architectural sandwich panels, whereas it would be ...
Cheung, YK, Chong, KP, Tham, LG
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The localized wrinkling instability, and the overall buckling of these panels due to axial compression and shear loading are presented. Numerically the finite strip method, the finite prism method, and the finite layer method are especially efficient in analyzing prismatic members such as these architectural sandwich panels, whereas it would be ...
Cheung, YK, Chong, KP, Tham, LG
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