A two dimensional interface element for coupling of independently modeled three dimensional finite element meshes and extensions to dynamic and non-linear regimes | 東京工業大学附属図書館文献データベース

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A two dimensional interface element for coupling of independently modeled three dimensional finite element meshes and extensions to dynamic and non-linear regimes

著者名:: Aminpour, Mohammad ( Old Dominion Univ. )
掲載資料名:: NASA Technical Reports
発行年:: 1995
号:: NASA-CR-199951
通号:: G3/02 0092322
パート:: NAS 1.26:199951
ペーパー番号:: N96-16984
開始ページ:: 1
終了ページ:: 18
総ページ数:: 18
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:	ZA00001432
論文注記:	NAG-1-1670

類似資料:

1 テクニカルペーパー A two-dimensional interface element for multi-domain analysis of independently modeled three-dimensional finite element meshes Aminpour, Mohammad A., Krishnamurthy, Thiagarajan American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Direct Formulation of a 4-Node Hybrid Shell Element With Rotational Degrees of Freedom Aminpour Mohammad, A. National Aeronautics and Space Adminstration
2 テクニカルペーパー Coupling of independently modeled three-dimensional finite element meshes with non-matching arbitrary shape interface boundaries Aminpour, Mohammad A., Krishnamurthy, Thiagarajan, Shin, Youngwon American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A 4-Node Assumed-Stress Hybrid Shell Element With Rotational Deress Of Freedom Aminpour, Mohammad A. National Aeronautics and Space Adminstration
3 テクニカルペーパー Thermal interface element for independently modeled finite element meshes Fadale, Tushar D., Aminpour, Mohammad a. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Finite element analysis of two-dimensional turbulent asymmetric near and far non-periodic and periodic wakes by K-E model of turbulence Nayak, Amlan Kusum, Venkatrayulu, N., Raj, D. Prithvi The American Society of Mechanical Engineers
4 テクニカルペーパー Finite element formulation of a three-node spatially curved and twisted beam Aminpour, Mohammad A., Padhye, Umesh V. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー IMPROVED ASSUMED-STRESS HYBRID SHELL ELEMENT WITH DRILLING DEGREES OF FREEDOM FOR LINEAR STRESS, BUCKLING, AND FREE VIBRATION ANALYSES Rengarajan, Govind, Aminpour, Mohammad A., Knight, Norman F., Jr. National Aeronautics and Space Adminstration
5 テクニカルペーパー Incongruent Interfaces in Three-Dimensional Finite Element Models MacNeal, R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー A Three Dimensional Finite Element Model for Emergency Response Wang, X., Pepper, D., Chen, Y., Hsieh, S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー A Generic Interface Element for COMET-AR McCleary, Suzan L., Aminpour, Mohammad A. National Aeronautics and Space Adminstration	12 テクニカルペーパー A Three-dimensional Finite Element Model of the Human Arm Palaniappan Jr.,Pal, Wipasuramonton,Paul, Begeman,Paul, Tanavde,Anand S., Zhu,Fuchun Society of Automotive Engineering, Inc.

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