The non-linear dynamic finite element analysis of composite cylindrical shells considering large rotations

The non-linear dynamic finite element analysis of composite cylindrical shells considering large rotations

著者名:

Gummadi, L.N.B. ( Department of Aeronautics and Astronautics, Air Force Institute of Technology, WPAFB, OH )
Palazotto, A.N. ( Department of Aeronautics and Astronautics, Air Force Institute of Technology, WPAFB, OH )

掲載資料名:

A collection of technical papers : 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, April 7-10, 1997, Kissimmee, FL

シリーズ名:

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

シリーズ巻号:

CP973

発行年:

1997

巻:

pt. 3

通号:

97-1234

ペーパー番号:

AIAA-97-1234

開始ページ:

2362

終了ページ:

2370

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563472275 [1563472279]

言語:

英語

請求記号:

(pt.1)A07400/970595,(pt.2)A07400/970596,(pt.3)A07400/970597,(pt.4)A07400/970598

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00006871
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum
回次:	38th
会議開催地:	Kissimmee, FL
会議開催年:	1997.04.07-1997.04.10

類似資料:

1 テクニカルペーパー Total Lagrangian approach to nonlinear finite element analysis of cylindrical shells considering large rotations Gummadi, L.N.B., Palazotto, A.N. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Finite Element Based Multi-Mode Initial Post-buckling Analysis of Composite Cylindrical Shells Rahman, T., Jansen, E. L. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Finite element analysis of low velocity impact on composite sandwich plates Palazotto, A.N., Herup, E.J., Gummadi, L.N.B. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Robustness Considerations in the Design of a Stabilizer Bar System. Soon, R.S., Gummadi, L.N.B., Cao, K.D. Society of Automotive Engineers
3 テクニカルペーパー Non-Linear Analysis of Tunable Compression Bushing for Stabilizer Bars. Fan, X., Cai, H., Lin, S., Gummadi, L.N.B., Cao, K. Society of Automotive Engineers	9 テクニカルペーパー Bushing Characteristics of Stabilizer Bars. Gummadi, L.N.B., Cai, H., Lin, S., Fan, X., Cao, K. Society of Automotive Engineers
4 テクニカルペーパー Low velocity impact damage characteristics of Z-fiber reinforced sandwich panels - an experimental study Palazotto, A.N., Gummadi, L.N.B., Vaidya, U.K., Herup, E.J. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Slave finite element for non-linear analysis of engine structures. Volume 2: Programmer's manual and user's manual Witkop, D. L., Dale, B. J., Gellin, S. National Aeronautics and Space Adminstration
5 テクニカルペーパー Buckling Analysis of Laminated Composite Circular Cylindrical Shells Harper,James G., Palazotto,Anthony N. Society of Automotive Engineering, Inc.	11 テクニカルペーパー Finite Element Analysis of Viscoelastic Elastomeric Structures Vibrating about Non-Linear Statically Stressed Configurations Morman Jr.,K.N., Kao,B.G., Nagtegaal,J.C. Society of Automotive Engineering, Inc.
6 テクニカルペーパー FINITE ELEMENT ANALYSIS OF GEOMETRICALLY NON-LINEAR PROBLEMS USING A COROTATIONAL LARGE ROTATION FORJMULATION MCIVOR, J.D.C., STEVEN, G.P. National Aeronautics and Space Adminstration	12 テクニカルペーパー Forced Non-linear Vibration of Cylindrical Laminated Shells by the p-version Finite Element Method Ribeiro, P. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12