TY - JOUR
T1 - Shape optimization of solid isotropic plates to mitigate the effects of air blast loading
AU - Argod, V.
AU - Nayak, S. K.
AU - Singh, A. K.
AU - Belegundu, A. D.
N1 - Funding Information:
This material is based upon work partly supported by the Army Research Office, Proposal Number 50490-EG, Monitored by Dr. Bruce LaMattina. We thank Dr. B.A. Cheeseman and Dr. C. Yen at ARL for valuable discussions on this project. Partial financial and computational support from the High Performance Computing Group at Penn State under Mr. Vijay Agarwala is gratefully acknowledged.
PY - 2010/7
Y1 - 2010/7
N2 - This article relates to the optimum shape of a solid isotropic plate to mitigate the effect of air blast loading, which comprises of a short duration pressure pulse. This article focuses on convergence aspects of the numerical procedure, well-posedness of the problem and effect of different boundary conditions. The plates are modeled using LS-DYNA with 3D hexahedral elements. The goal has been to minimize dynamic displacement while monitoring plastic strain values, mass, and envelope constraints. The optimum shape, a combination of deformation-based velocity fields, invariably results in a bottom bulge towards the charge. The shape of the top surface depends on various factors such as the mass limit and boundary conditions. Significant reduction in objective was achieved. Robust convergence of the numerical procedure is shown, as also the well-posedness of the problem formulation. A study with different boundary conditions along the edge has also been carried out.
AB - This article relates to the optimum shape of a solid isotropic plate to mitigate the effect of air blast loading, which comprises of a short duration pressure pulse. This article focuses on convergence aspects of the numerical procedure, well-posedness of the problem and effect of different boundary conditions. The plates are modeled using LS-DYNA with 3D hexahedral elements. The goal has been to minimize dynamic displacement while monitoring plastic strain values, mass, and envelope constraints. The optimum shape, a combination of deformation-based velocity fields, invariably results in a bottom bulge towards the charge. The shape of the top surface depends on various factors such as the mass limit and boundary conditions. Significant reduction in objective was achieved. Robust convergence of the numerical procedure is shown, as also the well-posedness of the problem formulation. A study with different boundary conditions along the edge has also been carried out.
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U2 - 10.1080/15397731003745428
DO - 10.1080/15397731003745428
M3 - Article
AN - SCOPUS:77955349688
SN - 1539-7734
VL - 38
SP - 362
EP - 371
JO - Mechanics Based Design of Structures and Machines
JF - Mechanics Based Design of Structures and Machines
IS - 3
ER -