A Consistent Configuration Formulation Involving Continuum Damage Mechanics Based Lagrangian Hydrodynamic Computational Framework for 3D High- and Hypervelocity Impact/Damage/Penetration Analysis

A Consistent Configuration Formulation Involving Continuum Damage Mechanics Based Lagrangian Hydrodynamic Computational Framework for 3D High- and Hypervelocity Impact/Damage/Penetration Analysis

著者名:

X. Zhou ( U.S. Army High Performance Computing Research Center, Minneapolis, MN )
D. Sha
K. Tamma ( University of Minnesota, Minneapolis, MN )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-1758

ペーパー番号:

AIAA Paper 2006-1758

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200606 [CD-ROM 2006 Disc 6]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047225
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Conference
回次:	47th ; 14th
会議開催地:	Newport, Rhode Island
会議開催年:	2006.05.01-2006.05.04

類似資料:

1 テクニカルペーパー A Computational Framework via the Continuum Damage Mechanics Based Model for Brittle Damage, and Numerical Validation with Experiment Y. Miller, X. Zhou, D. Sha, K. Tamma American Institute of Aeronautics and Astronautics	7 テクニカルペーパー On the Concept of Algorithms by Design with Illustrations to Computational Structural Mechanics/Dynamics Zhou, X., Tamma, K. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー An Explicit Computational Formulation for Frictional Contact/Impact Problems Zhou, X., Sha, D., Tamma, K. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Transient algorithms for heat transfer: theoretical developments and approaches for generating Nth-order accurate algorithms Tamma, K., Zhou, X., Sha, D. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー An Arbitrary Reference Configuration (ARC) Elasticity Theory and the Corresponding Stress Update Formulation for Finite Deformation Analysis Zhou, X., Tamma, K., Sha, D. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー An Optimal Family of Controllable Numerically Dissipative Time Integration Algorithms for Structural Dynamics Zhou,X., Tamma,K., Sha,D. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー An Arbitrary Reference Configuration (ARC) Based Nonlinear Shell Formulation for Finite Rotation/Deformation Dynamic Analysis Sha, Desong, Zhou, Xiangmin, Tamma, Kumar American Institute of Aeronautics and Astronautics	10 テクニカルペーパー A Novel Nonlinearly Explicit Secon-Order Accurate L-Stable Methodology for Finite Deformation Hypoelastic/Hypoelasto-Plastic Structural Dynamics Probl Tamma, K., Sha, D., Zhou, X. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Recent Developments in Linear/Nonlinear Computational Algorithms For Transient Heat Transfer Zhou,X., Tamma,K.K., Sha,D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー On the Measures for Evaluating Time Discretized Operators and the Consequences Leading to Improved Algorithms by Design for Structural Dynamics Zhou, X., Tamma, K., Sha, D. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー On the Significance and Impact of a Novel Design Framework Leading to Optimal Computational Algorithms Encompassing Linear Multi-Step Methods for Stru Tamma, K., Kanapady, R., Zhou, X. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Recent advances towards a virtual-pulse (VIP) time integral methodology for general structural dynamics problems: Theoretical developments and implementation … Tamma, K. K., Chen, X., Sha, D. The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12