Explicit Robust Schemes for Implementation of a Class of Principal Value-Based Constitutive Models: Symbolic and Numeric Implementation

Explicit Robust Schemes for Implementation of a Class of Principal Value-Based Constitutive Models: Symbolic and Numeric Implementation

著者名:

Arnold, S.M. ( National Aeronautics and Space Administration Lewis Research Center )
Saleeb, A.F.
Tan, H.Q.
Zhang, Y.

掲載資料名:

NASA Technical Reports

発行年:

1993

号:

NASA-TM-106124

パート:

NAS 1.15:106124

ペーパー番号:

N93-26946

開始ページ:

1

終了ページ:

55

総ページ数:

55

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001429

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1 テクニカルペーパー Explicit Robust Schemes for Implementation of General Principal Value-Based Constitutive Models Amold, S.M., Saleeb, A.F., Tan, H.Q., Zhag, Y. National Aeronautics and Space Adminstration	7 テクニカルペーパー A General Reversible Hereditary Constitutive Model Arnold, S. M., Saleeb, A. F., Castelli, M. G. National Aeronautics and Space Adminstration
2 テクニカルペーパー Explicit Rubust Schemes for Implementation of a Class of Principal Value- Based Constitutive Models: Theoretical Development Saleeb, A.F., Arnold, S.M. National Aeronautics and Space Adminstration	8 テクニカルペーパー On the Thermodynamic Framework of Generalized Coupled Thermoelastic-Viscoplastic-Damage Modeling Arnold, S.M., Saleeb, A.F. National Aeronautics and Space Adminstration
3 テクニカルペーパー Application of Symbolic Computations to the Constitutive Modeling of Structural Materials Arnold, Steven M., Tan, H.Q., Dong, X. National Aeronautics and Space Adminstration	9 テクニカルペーパー On the symbolic manipulation and code generation for elasto-plastic material matrices Chang, T. Y., Saleeb, A. F., Wang, P. S., Tan, H. Q. National Aeronautics and Space Adminstration
4 テクニカルペーパー Computer Simulation of the Mathematical Modeling Involved in Constitutive Equation Development: Via Symbolic Computations Arnold, S.M., Tan, H.O., Dong, X. National Aeronautics and Space Adminstration	10 テクニカルペーパー A Fully Associative, Nonisothermal, Nonlinear Kinematic, Unified Viscoplastic Model for Titanium Alloys Arnold, S.M., Saleeb, A.F., Castelli, M.G. National Aeronautics and Space Adminstration
5 テクニカルペーパー Calculation of stress intensity factors in an isotropic multicracked plate: Part 2: Symbolic/numeric implementation Arnold, S. M., Binienda, W. K., Tan, H. Q., Xu, M. H. National Aeronautics and Space Adminstration	11 テクニカルペーパー ON FINITE ELEMENT IMPLEMENTATION AND COMPUTATIONAL TECHNIQUES FOR CONSTITUTIVE MODELING OF HIGH TEMPERATURE COMPOSITES Final Report Saleeb, A. F. et al. National Aeronautics and Space Administration
6 テクニカルペーパー A Fully Associative, Non-Linear Kinematic, Unified Viscoplastic Model for Titanium Based Matrices Arnold, S.M., Saleeb, A.F., Castelli, M.G. National Aeronautics and Space Adminstration	12 テクニカルペーパー Robust integration schemes for generalized viscoplasticity with internal-state variables. Part 2: Algorithmic developments and implementation Li, Wei, Saleeb, Atef F. National Aeronautics and Space Adminstration

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