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Showing papers on "Timoshenko beam theory published in 1987"


Journal ArticleDOI
TL;DR: In this paper, it is shown that the Timoshenko beam can be uniformly stabilized by means of a boundary control, and a numerical study on the spectrum is also presented, showing that the beam is uniformly stabilized with respect to the boundary control.
Abstract: It is shown that the Timoshenko beam can be uniformly stabilized by means of a boundary control. A numerical study on the spectrum is also presented.

379 citations


Journal ArticleDOI
TL;DR: In this article, it was shown that the use of a first-order linear beam theory results in a spurious loss of bending stiffness, and that a geometrically non-linear (at least second-order) beam theory is sufficient to account for the influence of centrifugal force on bending stiffness.

185 citations


Journal ArticleDOI
01 Jul 1987
TL;DR: In this paper, the effect of a transverse surface crack on the free vibration of a rotor shaft and the influence of the crack on its vibrational behavior is investigated. But not all motions are coupled, however.
Abstract: A transverse surface crack is known to add to the shaft a local flexibility due to the stress-strain singularity in the vicinity of the crack tip. This flexibility can be represented by way of a 6 × 6 matrix describing the local flexibility in a short shaft element which includes the crack. This matrix has off-diagonal terms which cause coupling of motion along the directions which are indicated by the off-diagonal terms. Not all motions are coupled, however. To study the coupling of torsion and shear, a 3 × 3 flexibility matrix is used which includes the appropriate terms. Due to the shear terms of the Timoshenko beam equation of the shaft, bending vibration is finally coupled to torsional vibration. This effect is the subject of this investigation, which is of particular importance in turbomachinery operation. The equations of motion of a Timoshenko beam shaft with three degrees of freedom are derived. The free vibration of the shaft and the influence of the crack on the vibrational behaviour of the shaft is studied. The relation of the eigenvalues of the system, to the crack depth and the slenderness ratio of the shaft is derived. Moreover forced vibration analysis of the cracked shaft is performed. The significant influence of the bending vibration on the torsional vibration spectrum, and vice-versa, is demonstrated. It is believed that this effect can be very useful for rotor crack identification in service, which is of importance to turbomachinery.

112 citations


Journal ArticleDOI
TL;DR: In this article, the eigenvalue and lateral deflection of both the surface and middle plane of the plate, as well as the bending strains, are obtained in the form of series expansions in even powers of plate thickness.

98 citations


Journal ArticleDOI
TL;DR: In this article, the shear coefficient in Timoshenko beam theory is obtained for thin-walled beams constructed of laminated panels of composite material using a variation of the method due to Cowper.

86 citations


Journal ArticleDOI
TL;DR: In this paper, a co-rotational formulation combined with small deflection beam theory with the inclusion of the effect of axial force is adopted to distinguish between rigid body and deformational rotations.

66 citations


Journal ArticleDOI
TL;DR: In this paper, the influence of rotary inertia and shear deformation on the motion of a flexible robot arm modelled as a cantilevered Timoshenko beam with a lumped moment of inertia at the free end was determined.

62 citations


Journal ArticleDOI
TL;DR: In this article, the authors present two comprehensive analysis methodologies for composite beams and describe experimental results obtained from a thin-walled, rectangular cross-sectional beam, which are in good agreement with the observed twist and strain distributions.
Abstract: Beam theory is widely used as a first approximation in numerous structural applications. When applied to composite beams, the accuracy of beam theory becomes questionable because (1) the shearing and warping deformations become significant, as the shearing stiffness of composite laminates is often very low, and (2) several elastic couplings can occur that strongly influence the behavior of composite beams. The torsional behavior of thin-walled composite beams has important implications for aeronautical structures and is deeply modified by the above nonclassical effects. This paper presents two comprehensive analysis methodologies for composite beams and describes experimental results obtained from a thin-walled, rectangular cross-sectional beam. The theoretical predictions are found in good agreement with the observed twist and strain distributions. Out-of-plane torsional warping of the cross-section is found to be the key factor for an accurate modeling of the torsional behavior of such structures.

62 citations


01 Jul 1987
TL;DR: In this article, the so-called simple beam theory assumptions are examined to yield beam geometry ratios that will result in minimum error when utilizing elasticity theory, such as wedging stress, contact stress, load mislocation, beam twisting, friction at beam contact points, contact point tangency shift, and neglect of corner radii or chamfer in the stress determination.
Abstract: : Requirements for accurate bend-testing of four-point and three-point beams of rectangular cross-section are outlined. The so-called simple beam theory assumptions are examined to yield beam geometry ratios that will result in minimum error when utilizing elasticity theory. Factors that give rise to additional errors when determining bend strength are examined, such as: wedging stress, contact stress, load mislocation, beam twisting, friction at beam contact points, contact point tangency shift, and neglect of corner radii or chamfer in the stress determination. Also included are the appropriate Weibull strength relationships and an estimate of errors in the determination of the Weibull parameters based on sample size. Such analyses and results provide guidance for the accurate determination of flexure strength of brittle materials within the linear elastic regime. Error tables resulting from these analyses are presented.

58 citations


Journal ArticleDOI
Young-Pil Park1
TL;DR: In this paper, a finite element model of the beam transverse motion in the plane is formulated through the extended Hamilton's principle, and the dynamic stability of the model is studied with respect to (i) the location of the follower force direction control sensor, (ii) the sensor gain, (iii) the magnitudes of the rotary inertia and shear deformation parameters of a beam, and (iv) the magnitude of the constant follower force.

54 citations


Journal ArticleDOI
TL;DR: In this paper, a new mixed Petrov-Galerkin method is presented for the Timoshenko beam problem, allowing new combinations of interpolation, in particular, equal-order stress and displacement fields.
Abstract: A new mixed Petrov-Galerkin method is presented for the Timoshenko beam problem. The method has enhanced stability compared to the Galerkin formulation, allowing new combinations of interpolation, in particular, equal-order stress and displacement fields. The methodology is easily generalizable for multi-dimensional Hellinger-Reissner systems.

Journal ArticleDOI
TL;DR: In this article, an n-cycle iteration scheme is introduced to improve the convergence properties of the equilibrium iteration of the beam element in order to remove the restriction of small rotations between two successive increments for large displacement and large rotation analysis of space frames using incremental iterative methods.


01 Jan 1987
TL;DR: In this article, the standard means of representing finite rotation in rigid-body kinematics, including orientation angles, Euler parameters, and Rodrigues parameters, are reviewed and compared.
Abstract: Standard means of representing finite rotation in rigid-body kinematics, including orientation angles, Euler parameters, and Rodrigues parameters, are reviewed and compared. General kinematical relations for a beam theory that treats arbitrarily large rotation are then presented. The standard methods of representing finite rotations are applied to these kinematical expressions, and comparison is made among the standard methods and additional methods found in the literature, such as quasi-coordinates and linear combinations of projection angles. The method of Rodrigues parameters is shown to stand out for both its simplicity and generality when applied to beam kinematics, a result that is really missing from the literature.

Journal ArticleDOI
TL;DR: In this paper, a method for the dynamic analysis of flexible multibody systems that accounts for rotary inertia and shear deformation effects is presented, which is exemplified by a two-dimensional flexible multi-body aircraft.

Journal ArticleDOI
TL;DR: In this article, it is shown that the data triplets (λi, ui, θi)∞0 must satisfy certain inequalities and asymptotic trends if the reconstructed beam is indeed a slender beam, for which the Euler-Bernoulli beam theory holds.

Journal ArticleDOI
TL;DR: In this article, a beam theory which accounts for cross-sectional warping caused by transverse shearing is presented, and a stress resultant theory is formulated for elastic beams, and examples are provided to assess the effects of warping restraint.
Abstract: A beam theory which accounts for cross-sectional warping caused by transverse shearing is presented. A stress resultant theory is formulated for elastic beams, and examples are provided to assess the effects of warping restraint. The ideas are extended to the case of elastoplastic warping. A numerical formulation for the analysis of the inelastic problem is presented and examples of elastoplastic warping are given.


Journal ArticleDOI
01 Mar 1987
TL;DR: In this article, a finite element technique is used to obtain the natural frequencies and transient responses of Timoshenko beams resting on elastic foundations, where the beam is discretized into beam elements, each with four degrees of freedom.
Abstract: A finite element technique is used to obtain the natural frequencies and transient responses of Timoshenko beams resting on elastic foundations The beam is discretized into beam elements, each with four degrees of freedom The equations of motion in terms of the nodal degrees of freedom are derived by applying Hamilton's principle The numerical results for a hinged-hinged beam are given to show the effects of rotatory inertia, shear deformation and foundation constants on the natural frequencies of the beam The transient responses of beams are subsequently presented and compared with the available solutions

Journal ArticleDOI
TL;DR: In this article, the authors present a method for predicting the fatigue life of flexible offshore platforms, which takes into account the nonlinearities in the waves and the stochastic nature of the sea.

Journal ArticleDOI
TL;DR: Petrov-Galerkin formulations of the Timoshenko beam problem are presented in this paper, which provide the best approximation property, optimal rate of convergence, and nodally exact solution for arbitrary loading, for all values of the thickness of the beam.
Abstract: Petrov-Galerkin formulations of the Timoshenko beam problem are presented. They are shown to provide the best approximation property, optimal rate of convergence, and nodally exact solution for arbitrary loading, for all values of the thickness of the beam.

Journal ArticleDOI
TL;DR: In this article, the fundamental frequency of vibration (antisymmetric mode) of a frame elastically restrained against translation and rotation at the ends, carrying concentrated masses, was determined by means of the Rayleigh-Ritz method and simple polynomial coordinate functions in order to represent the displacement field.

01 Jan 1987
TL;DR: In this article, boundary feedback schemes for stabilizing flexural vibrations in a linear viscoelastic beam are studied, and it is shown that in the EulerBernoulli model an arbitrarily small feedback delay can cause unbounded vibrations with arbitrarily large exponential growth rates.
Abstract: Boundary feedback schemes for stabilizing flexural vibrations in a linear viscoelastic beam are studied. It is shown that in the EulerBernoulli model an arbitrarily small feedback delay can cause unbounded vibrations with arbitrarily large exponential growth rates. For the Timoshenko beam: in the purely elastic case: a contrasting result is given, and formulas for decay rates of high frequency modes are developed for the case of no feedback delay. Numerical results for various no-delay cases are summarized.

Book ChapterDOI
01 Jan 1987
TL;DR: In this paper, Bickford used Hamilton's principle to derive a consistent, higher order theory for the elastodynamics of beams based upon the kinematic and stress assumptions previously used by Levinson [2] for beams of rectangular cross-section.
Abstract: In 1982 Bickford [1] used Hamilton’s principle to derive a consistent, higher order theory for the elastodynamics of beams based upon the kinematic and stress assumptions previously used by Levinson [2] for beams of rectangular cross-section. In [2] the usual beam equations of motion [3] were used to obtain a higher order beam theory. This latter theory provided a fourth order system of differential equations not too unlike the equations of Timoshenko beam theory with a difference being that in Levinson’s theory the shear stress boundary conditions on the lateral surfaces of the beam were satisfied. Bickford’s variationally consistent theory consists of a sixth order system of differential equations requiring the specification, provided by the variational formulation, of three boundary conditions at each end of the beam. A vectorial formulation of Bickford’s theory is achieved in [1] by defining a posteriori, a “...higher order moment resultant” but, as Bickford himself notes, “it remains to be seen whether or not there can be developed a rational method for constructing the vectorial equations without knowing, a priori, the variational equations.” This latter point is of no consequence since the validity of the variational equations is unquestioned.

01 Jan 1987
TL;DR: In this paper, the development of a finite strip analysis of thin-walled section buckling behavior is outlined, and the analysis uses plate theory for out of plane deflection behaviour and beam theory for in plane displacement behaviour.
Abstract: The development of a finite strip analysis of thin-walled section buckling behaviour is outlined. The analysis uses plate theory for out of plane deflection behaviour and beam theory for in plane displacement behaviour, and is suitable for use on microcomputers. A number of typical buckling problems are examined to illustrate the general applicability of the method, and the results are discussed.

Journal ArticleDOI
TL;DR: In this article, a set or governing equations for the linear theory of a circular cylindrical shell such as tanks and silos is presented explicitly from rod theory including the distortion of the transverse cross-section.

Proceedings ArticleDOI
01 Dec 1987
TL;DR: In this paper, boundary feedback schemes for stabilizing flexural vibrations in a linear viscoelastic beam are studied, and it is shown that in the Euler-Bernoulli model an arbitrarily small feedback delay can cause unbounded vibrations with arbitrarily large exponential growth rates.
Abstract: Boundary feedback schemes for stabilizing flexural vibrations in a linear viscoelastic beam are studied. It is shown that in the Euler-Bernoulli model an arbitrarily small feedback delay can cause unbounded vibrations with arbitrarily large exponential growth rates. For the Timoshenko beam, in the purely elastic case, a contrasting result is given, and formulas for decay rates of high frequency modes are developed for the case of no feedback delay. Numerical results for various no-delay cases are summarized.

Journal ArticleDOI
TL;DR: In this article, the authors demonstrate the mechanics of these concepts using the simplest shear: flexible beam element (linear Timoshenko beam element) as13; exilayle, and verily its apriori projections through digital computations.

Journal ArticleDOI
TL;DR: In this paper, a mixed implicit-explicit scheme is proposed as a technique for circumventing this restriction, and it is shown that this scheme is equivalent to an approach suggested by Belytschko and Mindle9.
Abstract: A brief summary of recent developments in numerical methods for doing transient analyses of Timoshenko and Mindlin types of structures is given. The pure shearing behaviour of these structures (with no transverse motion) is identified as the high-frequency mode which severely restricts the time step in standard explicit time integration methods. A mixed implicit–explicit scheme is proposed as a technique for circumventing this restriction, and it is shown that this scheme is equivalent to an approach suggested by Belytschko and Mindle9.

Book ChapterDOI
01 Jan 1987
TL;DR: The most important refined effect is shear deformation, followed by the effects of rotary ineria, axial prestress etc. as mentioned in this paper, which is the most important effect for beam-like structures.
Abstract: The calculation of the natural frequencies, modes and dynamical responses of beam-like structures is an important subject in structural dynamics sciences. In a lot of practical cases, it is sufficient to base these calculations on the classical EULER-BERNOULLI beam theory. However, equally numerous cases exist where it is necessary to take into account refined effects that exceed the classical theory to ensure a right description of the behaviour of the beam. The most important refined effect is that of shear deformation, followed by the effects of rotary ineria, axial prestress etc.