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This study is the first work to consider the sound radiation of a panel subject to 2 1 internal resonance.
The damage mechanisms of the sandwich panel subject to quasi-static indentation and perforation were analyzed through the numerical models.
This work deals with the problem of the least-weight design of a composite stiffened panel subject to constraints of different nature (mechanical, geometrical and manufacturability requirements).
This work presents a detailed procedure for flexural testing, on two spans, of simply supported full wood-based sandwich panel subject to uniform load.
These controllers are implemented on a tapered and swept aluminium panel subject to random excitation, such that the first five modes are simultaneously observed and controlled.
In the present study the effect of fiber orientation is studied on the failure load of a laminated curved panel subject to uniaxial compression.
Similar(48)
Damage tolerance has been studied experimentally with the panel subjected to impact damage.
The shielding properties of honeycomb sandwich panel subjected to high-velocity impact is of great concern to spacecraft design.
The panel subjected to punching load failed in flexural mode, and its behavior is similar to conventional RC slab.
The stability of stiffened composite curved panel subjected to shear and in-plane bending was analyzed by the obtained data.
Local facesheet buckling of a curved sandwich panel subjected to external pressure pulse loading was investigated in this paper.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com