Computer analysis of various shells of revolution.
Buckling of shells of revolution under axisymmetrical loading analyzed by computer program
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Buckling of shells of revolution under axisymmetrical loading analyzed by computer program
Adhesive, which bonds a metal liner to a filament wound composite structure used for cryogenic pressure vessels, prevents the metal liner from buckling under depressurization. The adhesive consists of adducts of urethane and epoxy resins.
Mathematical programming in optimized truss design noting reduction of components under buckling
Flutter analysis of plates with inplane boundary support flexibility exposed to transverse pressure loading or buckled by uniform thermal expansion
Flutter design charts for isotropic panels stressed to verge of buckling for typical values of structural damping
Linear static deformation and buckling of shallow spherical shells under asymmetric load by solving two dimensional finite difference equations
Device welds fine gage wire 0.001-in. in diameter. It permits welding of thermocouple junctions of the same size with straight sections adjacent to the junctions. Electrode arrangement provides constant pressure on the joint during welding while fully supporting the wires to prevent buckling or movement.
Energy method analysis establishes parameters governing stability of circular rings acted upon by constant, uniformly distributed loads. Energy method is used so that nonlinear behavior of structure before buckling can be accounted for. Method affords conceptually superior basis for analyzing the axisymmetric deviation mode.
Burst disk/cutter, prewelded before assembly, eliminates external leakage into a vacuum annulus and provides a means for more accurate burst-pressure prediction. Two reverse buckling type configurations are described and test results are given.
High speed photography for instability onset and subsequent buckling process in photoelastic circular cylindrical shells under axial compression
Critical load and instability of smooth and mesh surface mechanical systems subjected to impinging fluid jet, noting static buckling and flutter effects
Optimal inextensional buckling of uniformly loaded simply supported arches with large opening angle
Nonlinear dynamic analysis of shells of revolution under symmetric and asymmetric loads, obtaining solutions for shallow cap buckling
Flutter design charts for isotropic panels stressed to verge of buckling for tropical values of structural damping
Circular cylindrical shell stability under axial compressive load, analyzing buckling process by high speed photographic recording of photoelastic isoclinic pattern changes
Thin walled shells structural vibration, buckling and stress analysis by computer methods, discussing shell theory and design
Multilevel analysis computer program is useful in fiber matrix composites diagnosis, in structural syntheses of multilayered thornel/epoxy composite plates, in buckling studies of simply supported multilayered fiber composite plates, and in computing lamination residual stresses in angle ply composites.
Device, consisting of tongue of thin aluminum alloy strip, pull tab, slotted steel plate which serves as cutter, and steel buckle, absorbs mechanical energy when its ends are subjected to tensile loading. Device is applicable as auxiliary shock absorbing anchor for automobile and airplane safety belts.