Results 231 to 240 of about 10,312 (268)
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Buckling of Sandwich Cylinders Under Axial Load
Journal of the Aerospace Sciences, 1962This paper presents the solution for the nonlinear postbuckling behavior of a cylindrical sandwich shell with face sheets of a homogeneous material and a core of an isotropic shear-resistant material. Effects of inelastic behavior are neglected. The principle of minimum potential energy is used in the derivation of the compatibilit}^ equation.
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Buckling Loads of Beams or Plates on Continuous Supports
Journal of the Aeronautical Sciences, 1944Not ...
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ON DEFORMATIONS OF ELASTIC COLUMNS NEAR THE BUCKLING LOAD
The Quarterly Journal of Mechanics and Applied Mathematics, 1966Unter der kritischen Last erleidet ein nicht ideal gerader Stab bekanntlich unendlich große Ausbiegungen. Verf. diskutiert den besonderen Fall, daß die Form \(y_0(x)\) des vorgebogenen Stabes orthogonal zur Knick-Form ist -- jetzt bleiben die Ausbiegungen endlich.
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Buckling Behavior Above the Tangent Modulus Load
Journal of the Engineering Mechanics Division, 1961Inelastic buckling behavior of concentrically loaded strut having reduced rectangular cross section as mid-section; buckling model is similar to that originally used by F.R.Shanley, but in present model, solid rectangular cross section is introduced which permits detailed exploration of stress distribution across section; influence of slight ...
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Determination of the Buckling Load for Columns of Variable Stiffness
Journal of Applied Mechanics, 1949Abstract A method is given for determining both upper and lower bounds on the critical or buckling load for variable-section columns with axial loading. This method, which is an extension of the Rayleigh principle, is illustrated by three examples.
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Discussion of “Silverman on Buckling Loads”
Transactions of the American Society of Civil Engineers, 1951I. K. Silverman +4 more
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The Computation of Flexural–Torsional Buckling Loads
Journal of Applied Mechanics, 1952Abstract Solution by ordinary means of the cubic equation for the torsional buckling load, first derived by Kappus, often leads to insufficiently accurate results. A method is presented which avoids the loss of accuracy involved. The procedure is straightforward and no graphical means are involved. However, one formula is to be solved by
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Prediction of Buckling Load from Vibration Measurements
2002The linear relationship between buckling load and the square of the frequency of a structure is limited to the cases in which the fundamental vibration mode and the lowest buckling mode are the same. For cases where the two modes are different researchers in the past have suggested some empirical equations.
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