Analytical and experimental investigation of end-plane rotations of truncated cones under bending loads
Beam stiffness determined for thin walled truncated cones under bending loads
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Beam stiffness determined for thin walled truncated cones under bending loads
Postbuckling behavior and subsequent imperfection sensitivity of thin walled cylinders subjected to torsion, considering perturbation
Buckling load of cylindrical shell with inclined stiffeners, using method for stability of thin walled cylinder under transverse end load at free end
Steady state flux jumping for thin walled tubular superconducting NbTi subjected to coaxial superimposed AC and DC magnetic fields, discussing effective resistivity
Empirical technique predicts failure loads for centrally loaded columns with thin-walled, open cross sections. Interaction of two failure modes is predicted by modification of the Johnson-Euler equation.
Plastic deformation and crack opening displacement in thin walled, cylindrical shells
Thin walled metal cylinders residual deformation microstructures under internal impulsive loading
Thin plates and thin walled cylinders aeroelastic stability in fluid flow, analyzing panel flutter
Thin walled shells structural vibration, buckling and stress analysis by computer methods, discussing shell theory and design
Manufacturing process produces molybdenum foil 0.002 cm thick and 305 m long, and forms foil into high-strength, thin-walled tubing which can be flattened for storage on a spool. Desirable metal properties include high thermal conductivity stiffness, yield and tensile stress, and low thermal expansion coeffecient.
Sealed separable connection for thin wall metal tube
Stress analysis of elastic plate, composite plates with holes, fiber reinforced plates, and thin walled shells
Computer program for hydroelastic analysis of thin walled structures
Stress wave emission from subcritical crack growth in thin walled Al-V titanium alloy
Thermode composed of two thin-walled stainless steel hypodermic needles and cooper-constantan thermocouple or small thermistor to indicate temperature at point of perfusion is used to measure brain temperature in animals. Because of relatively small size of thermode, structural damage to brain is minimized.
The normal mode vibration characteristics of one-dimensional and two-dimensional panel arrays were investigated analytically and experimentally. The finite element displacement method was used to formulate the structural models. The structural models include a stiffness and consistent mass matrix for thin-walled open-section beams not previously reported, and a modification of a rectangular plate bending element to include a fundamental interior mode for the element as a generalized coordinate. Provision for adding lumped masses to represent accelerometers is also included. For the one-dimensional panel, the normal mode stress resultants are obtained by integrating the equilibrium equations directly. For the two-dimensional panel arrays, the solution for the stress resultants in the cover sheet was attempted by introducing stress functions dependent upon the displacement field of the plate element. This approach, although incomplete, is a natural extension of the one-dimensional analysis for plate elements. The exerimental program which was used to verify the analysis is described and experimental results are compared with the analysis.
The Apollo 15 soil-mechanics experiment has offered greater opportunity for study of the mechanical properties of the lunar soil than previous missions, not only because of the extended lunar-surface stay time and enhanced mobility provided by the lunar roving vehicle (rover), but also because four new data sources were available for the first time. These sources were: (1) the self-recording penetrometer (SRP), (2) new, larger diameter, thin-walled core tubes, (3) the rover, and (4) the Apollo lunar-surface drill (ALSD). These data sources have provided the best bases for quantitative analyses thus far available in the Apollo Program.
Axisymmetric responses are presented of a nonshallow thin-walled spherical shell on the basis of nonlinear bending theory. An ordinary differential equation with nonlinearity of quadratic as well as cubic terms associated with variable time is derived. The derivation is based on the assumption that the deflection mode is the sum of four Legendre polynomials, and the Galerkin procedure is applied. The equation is solved by asymptotic expansion, and a first approximate solution is adopted. Unstable regions of this solution are discussed.