deformable mesh
Recently Published Documents


TOTAL DOCUMENTS

47
(FIVE YEARS 1)

H-INDEX

12
(FIVE YEARS 0)

2021 ◽  
pp. 102181
Author(s):  
Megumi Nakao ◽  
Kotaro Kobayashi ◽  
Junko Tokuno ◽  
Toyofumi Chen-Yoshikawa ◽  
Hiroshi Date ◽  
...  

Author(s):  
Dumitri Silviu Perijoc ◽  
Leonard Domnişoru ◽  
Cristi Marian Angheluta

"As part of the continuum growth of the shipping industry, new challenges arise for the engineers. The development of floating structures capable of withstanding accidental loads, such as grounding and ship collisions, become nowadays an integral part of the design process. The current paper presents a methodology for impact analysis using FEMAP software capabilities in two distinct stages. The first stage consists of the impact analysis using a rigid indenter displaced at different speeds. The second stage of the study evaluates the impact analysis considering both the indenter and the structure deformable. Mesh influence tests, as well as the influence of the type of elements used in the analysis, have been taken into consideration in the present study."


Author(s):  
Tuan T. Nguyen ◽  
Vedrana A. Dahl ◽  
J. Andreas Barentzen ◽  
Anders B. Dahl

2019 ◽  
Vol 117 ◽  
pp. 97-103 ◽  
Author(s):  
Tuan T. Nguyen ◽  
Vedrana A. Dahl ◽  
J. Andreas Bærentzen

2017 ◽  
Vol 1 (2) ◽  
pp. 147-157 ◽  
Author(s):  
Felipe M. Parages ◽  
Thomas S. Denney ◽  
Himanshu Gupta ◽  
Steven G. Lloyd ◽  
Louis J. Dell'Italia ◽  
...  

2014 ◽  
Vol 1036 ◽  
pp. 568-573
Author(s):  
Florin Oloeriu ◽  
Oana Mocian ◽  
Roxana Nedelcu ◽  
Dănuţ Grosu ◽  
Constantin Ilie

The ballistic simulation attempted in this work is among the most difficult as both the projectile and the target experience significant deformations. Traditionally these simulations have been performed using a Lagrangian approach, i.e. a deformable mesh with large mesh deformations. There are three often used techniques when studying ballistic problems with the Lagrangian method: remeshing (generally not available for 3D hexahedra meshes), the 'pilot hole' technique and material erosion. Because these techniques imply element removal, in order to allow the calculation to continue, the Lagrangian method lacks a physical basis. Moreover, no general guidance exists for selecting one of the three techniques mentioned before. The Smoothed Particle Hydrodynamic method as implemented in the commercial code LS-DYNA has been used in this paper to solve the problem of the impact between different caliber projectiles and various types of metal targets. The results are compared to those produced by dynamic analysis using conventional finite element methods with material erosion as implemented in LS-DYNA.


Sign in / Sign up

Export Citation Format

Share Document