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 p
Numerical simulation of the ground effect using the boundary element method
โ Scribed by Katsuhiro Kikuchi; Fuminori Motoe; Mitsunori Yanagizawa
- Publisher
- John Wiley and Sons
- Year
- 1997
- Tongue
- English
- Weight
- 455 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0271-2091
No coin nor oath required. For personal study only.
โฆ Synopsis
As is well known, the lift of a wing passing over the ground becomes larger than that of a wing in a ยฎnite air ยฎeld 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 investigations were conducted to calculate the unsteady aerodynamic forces for long and short ground plates by means of boundary element techniques. In order to calculate the pressure variation on a long ground plate, the steady boundary element method was used. However, when using a short ground plate, the boundary element method was modiยฎed to treat the unsteady aerodynamic phenomena. Experimental studies were also made for both ground plates to conยฎrm the validity of the numerical results. At low angles of attack the qualitative behaviour of the unsteady aerodynamic pressure on both ground plates was well predicted by the boundary element methods and qualitative agreement is found between the calculated and measured results.
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