Development of Curved-Plate Elements for the Exact Buckling Analysis of Composite Plate Assemblies Including Transverse-Shear Effects
The analytical formulation of curved-plate non-linear equilibrium equations including transverse-shear-deformation effects is presented. A unified set of non-linear strains that contains terms from both physical and tensorial strain measures is used. Linearized, perturbed equilibrium equations (stability equations) that describe the response of the plate just after buckling occurs are derived. These equations are then modified to allow the plate reference surface to be located a distance z(sub c) from the centroidal surface. The implementation of the new theory into the VICONOPT exact buckling and vibration analysis and optimum design compute…
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Produktdetails
Weitere Autoren: National Aeronautics And Space Administr (Hrsg.)
- ISBN: 978-1-288-91048-9
- EAN: 9781288910489
- Produktnummer: 39580707
- Verlag: BiblioScholar
- Sprache: Englisch
- Erscheinungsjahr: 2013
- Seitenangabe: 116 S.
- Masse: H24.6 cm x B18.9 cm x D0.6 cm 222 g
- Gewicht: 222
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