5,425 research outputs found
LOWER BOUNDS FOR THE BUCKLING PRESSURE OF SPHERICAL SHELLS
Hydrostatic buckling pressure calculations for spherical shell
An experimental study of the buckling of complete spherical shells
Buckling of complete spherical shells to examine Tsien energy hypothesi
The inward bulge type buckling of monocoque cylinders I : calculation of the effect upon the buckling stress of a compressive force, a nonlinear direct stress distribution, and a shear force
In the present part I of a series of reports on the inward bulge type buckling of monocoque cylinders the buckling load in combined bending and compression is first derived. Next the reduction in the buckling load because of a nonlinear direct stress distribution is determined. In experiments nonlinearity may result from an inadequate stiffness of the end attachments in actual airplanes from the existence of concentrated loads or cut-outs. The effect of a shearing force upon the critical load is investigated through an analysis of the results of tests carried out at GALCIT with 55 reinforced monocoque cylinders. Finally, a simple criterion of general instability is presented in the form of a buckling inequality which should be helpful to the designer of a monocoque in determining the sizes of the rings required for excluding the possibility of inward bulge type buckling
Stresses in and general instability of monocoque cylinders with cutouts V : calculation of the stresses in cylinders with side cutout
Numerical Procedures for the Calculation of the Stresses in Monocoques II : Diffusion of Tensiles Stringer Loads in Reinforced Flat Panels with Cut-outs
Stresses in and General Instability of Monocoque Cylinders with Cutouts I : Experimental Investigation of Cylinders with a Symmetric Cutout Subjected to Pure Bending
Ten 24S-T alclad cylinders of 20-inch diameter, 45- or 58-inch length, and 0.012-inch wall thickness, reinforced with 24S-T aluminum alloy stringers and rings were tested in pure bending. In the middle of the compression side of the cylinders there was a cutout extending over 19 inches in the longitudinal direction, and over an angle of 45 degrees, 90 degrees, or 135 degrees in the circumferential direction. The strain in the stringers and in the sheet covering was measured with metal electric strain gages. The stress distribution in the cylinders deviate considerably from the linear law valid for cylinders without a cutout. The maximum strain measured was about four-thirds of the value calculated from the Mc/I formula when I was taken as the moment of inertia of the cross section of the portion of the cylinder where the cutout was situated. A diagram is presented containing the strain factors defined as the ratios of measured strain to strain calculated with the Mc/I formula. All the 10 cylinders tested failed in general instability. Two symmetric and one antisymmetric pattern of buckling were observed and the buckling load appeared to be independent of the method of manufacture and the length of the cylinder. The buckling load of the cylinders having cutouts extending over 45 degrees, 90 degrees, and 135 degrees was 66, 47, and 31 percent, respectively, of the buckling load of the cylinder without a cutout
Geotecnologias nos estudos geológicos e geotécnicos para suporte à gestão ambiental no litoral norte do RS (Brasil): um panorama de duas décadas.
O objetivo deste trabalho foi comparar os dados disponÃveis, bem como as técnicas e os softwares utilizados há duas décadas frente ao que hoje está disponÃvel para produzir mapas temáticos, empregando dados vetoriais e de imagens e integrando os mesmos num sistema de informações geográficas (SIG)
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