Typically, the cantilever non-uniform gravity-loaded Euler-Bernoulli beams are numerically modeled as the governing equation for free vibration analysis does not yield an exact solution. We show that, for certain polynomial variations of the mass and stiffness, there exists a fundamental closed form solution to the fourth order governing differential equation for gravity-loaded beams. An inverse problem approach is used to find an infinite number of such beams, with various mass and stiffness distributions, which share the same fundamental frequency. The derived distributions are demonstrated as test functions for a p-version finite element method. The functions can also be used to design gravity-loaded cantilever beams having a pre-specifi...
The paper deals with the construction of a stochastic reduced-order model for beam-like dynamical st...
The selection criteria for Euler-Bernoulli or Timoshenko beam theories are generally given by means ...
The random vibration analysis of aircraft structural components is often performed with simplified t...
Typically, the cantilever non-uniform gravity-loaded Euler-Bernoulli beams are numerically modeled a...
Typically, numerical or approximate methods are used for the free vibration analysis of axially load...
The paper introduces an extreme value model based on statistical moments to predict modal and vibrat...
Rotating and non-rotating beams are widely used to model important engineering struc-tures. Hence, t...
This article enhances the discrete singular convolution method for free vibration analysis of non-un...
Abstract. The consideration of uncertainties in numerical models to obtain the probabilistic descrip...
The full text of this article will not be available in ULIR until the embargo expires on the 28/10/2...
In this paper, the stiffness and mass per unit length distributions of a rotating beam, which is iso...
An exact solution for the title problem is obtained using the Bernoulli-Euler theory of beam vibrati...
The von Mises stress is often used as the metric for evaluating design margins, particularly for str...
Beam on an elastic foundation represents many applications like bridges, rail tracks. The analysis o...
A finite element-based methodology is developed for the determination of the dynamic stiffness matri...
The paper deals with the construction of a stochastic reduced-order model for beam-like dynamical st...
The selection criteria for Euler-Bernoulli or Timoshenko beam theories are generally given by means ...
The random vibration analysis of aircraft structural components is often performed with simplified t...
Typically, the cantilever non-uniform gravity-loaded Euler-Bernoulli beams are numerically modeled a...
Typically, numerical or approximate methods are used for the free vibration analysis of axially load...
The paper introduces an extreme value model based on statistical moments to predict modal and vibrat...
Rotating and non-rotating beams are widely used to model important engineering struc-tures. Hence, t...
This article enhances the discrete singular convolution method for free vibration analysis of non-un...
Abstract. The consideration of uncertainties in numerical models to obtain the probabilistic descrip...
The full text of this article will not be available in ULIR until the embargo expires on the 28/10/2...
In this paper, the stiffness and mass per unit length distributions of a rotating beam, which is iso...
An exact solution for the title problem is obtained using the Bernoulli-Euler theory of beam vibrati...
The von Mises stress is often used as the metric for evaluating design margins, particularly for str...
Beam on an elastic foundation represents many applications like bridges, rail tracks. The analysis o...
A finite element-based methodology is developed for the determination of the dynamic stiffness matri...
The paper deals with the construction of a stochastic reduced-order model for beam-like dynamical st...
The selection criteria for Euler-Bernoulli or Timoshenko beam theories are generally given by means ...
The random vibration analysis of aircraft structural components is often performed with simplified t...