As is well known, the lift of a wing passing over the ground becomes larger than that of a wing in a ®nite air ®eld because of the ground effect. Owing to its special aerodynamic characteristics and applications, the problem of the ground effect has become increasingly common. In this paper some inv
Numerical simulations of impacts using a discrete element method
✍ Scribed by S. A. Magnier; F. V. Donzé
- Publisher
- John Wiley and Sons
- Year
- 1998
- Tongue
- English
- Weight
- 287 KB
- Volume
- 3
- Category
- Article
- ISSN
- 1082-5010
No coin nor oath required. For personal study only.
✦ Synopsis
Impacts of rigid spherical nose shaped missiles on concrete beams are simulated with a discrete element method. The history of the structural damage of the beam is followed from the very first crushing and fracturing processes to the ultimate fragmentation step. Spalling, scabbing, penetration and perforation events are characterized and compared with real test cases of the civil engineering industry. It is found that these phenomena depend not only on the kinetic energy of the missile as predicted by some recent empirical laws but also on its momentum. This means that the dynamic impact loading time is determinant in the scabbing and perforation thicknesses. When the numerical data is plotted against the empirical rules determined from experimental data, the fit is good although the model is two dimensional.
1998 John Wiley & Sons, Ltd.
📜 SIMILAR VOLUMES
A novel approach in analysing the vibration of elastic body systems is presented and discussed in this paper. This method uses a meshless spatial approximation based only on nodes, which constitutes an advantage over the "nite element method. As it is applicable to an elastic body with arbitrary sha
The present paper makes use of a wave equation formulation of the primitive shallow water equations to simulate one-dimensional free surface flow. A numerical formulation of the boundary element method is then developed to solve the wave continuity equation using a time-dependent fundamental solutio
The behaviour of a premixed turbulent ame is numerically studied in this paper. The numerical model is based on solving turbulent ow ÿeld by the discrete vortex method. The ame is considered to be of zero thickness boundary which separates burnt and unburnt regions with di erent constant density and