TY - GEN
T1 - Ordinary-state based peridynamic truss element
AU - Dorduncu, M.
AU - Barut, A.
AU - Madenci, E.
N1 - Publisher Copyright:
© American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2015
Y1 - 2015
N2 - This study presents a truss element that accounts for the peridynamic interactions among the finite element nodes. However, these interactions result in a sparsely populated global system stiffness matrix. Therefore, the skyline technique is used in the solution of resulting system of equations until damage initiates; then the explicit time integration to monitor damage progression. The major advantage of this element is the construction of the solution immediately before failure occurs with much less computational effort. In the absence of failure, the predictions from the peridynamic truss element are verified against finite element analysis with traditional elements. Also, a plate with a hole under tension is considered to demonstrate crack initiation and its propagation.
AB - This study presents a truss element that accounts for the peridynamic interactions among the finite element nodes. However, these interactions result in a sparsely populated global system stiffness matrix. Therefore, the skyline technique is used in the solution of resulting system of equations until damage initiates; then the explicit time integration to monitor damage progression. The major advantage of this element is the construction of the solution immediately before failure occurs with much less computational effort. In the absence of failure, the predictions from the peridynamic truss element are verified against finite element analysis with traditional elements. Also, a plate with a hole under tension is considered to demonstrate crack initiation and its propagation.
UR - http://www.scopus.com/inward/record.url?scp=85088356756&partnerID=8YFLogxK
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U2 - 10.2514/6.2015-0465
DO - 10.2514/6.2015-0465
M3 - Conference contribution
AN - SCOPUS:85088356756
T3 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
BT - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
Y2 - 5 January 2015 through 9 January 2015
ER -