Results 131 to 140 of about 4,330 (212)

Sizing-stiffened composite panels loaded in the postbuckling range [PDF]

open access: yes
Stiffened panels are widely used in aircraft structures such as wing covers, fuselages, control surfaces, spar webs, bulkheads, and floors. The detailed sizing of minimum-weight stiffened panels involves many considerations.
Biggers, S. B., Dickson, J. N.
core   +1 more source

Buckling Testing and Analysis of Honeycomb Sandwich Panel Arc Segments of a Full-Scale Fairing Barrel Part 4: Six-ply Out-of-Autoclave Facesheets [PDF]

open access: yes
Four honeycomb sandwich panel types, representing 1/16th arc segments of a 10-m diameter barrel section of the Heavy Lift Launch Vehicle (HLLV), were manufactured and tested under the NASA Composites for Exploration program and the NASA Constellation ...
Dixon, Genevieve D.   +4 more
core   +1 more source

A finite element procedure for nonlinear prebuckling and initial postbuckling analysis [PDF]

open access: yes
A procedure cast in a form appropriate to the finite element method is presented for geometrically nonlinear prebuckling and postbuckling structural analysis, including the identification of snap-through type of buckling.
Gallagher, R. H., Mau, S. T.
core   +2 more sources

Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects [PDF]

open access: yes
Buckling and postbuckling results are presented for compression-loaded simply-supported aluminum plates and composite plates with a symmetric lay-up of thin + or - 45 deg plies composed of many layers.
Librescu, Liviu   +2 more
core   +1 more source

Material Design for Optimal Postbuckling Behaviour of Composite Shells. [PDF]

open access: yesMaterials (Basel), 2021
Magisano D   +4 more
europepmc   +1 more source

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