Approximate Solution and Optimum Design for Postbuckling of Infinite Laminated Composite Plates Subjected to Compression Loading

Approximate Solution and Optimum Design for Postbuckling of Infinite Laminated Composite Plates Subjected to Compression Loading

著者名:

Diaconu, C. ( University of Bristol, Bristol, Great Britain )
Weaver, P.

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:

45th

発行年:

2004

通号:

2004-1565

ペーパー番号:

AIAA-2004-1565

出版情報:

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

ISSN:

10877215

言語:

英語

請求記号:

A07400/200406 [CD-ROM 2004 Disc 6]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001601
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
回次:	45th
会議開催地:	Palm Springs, California
会議開催年:	2004.04.19-2004.04.22

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1 テクニカルペーパー Postbuckling of Long Laminated Composite Plates with Unsymmetric Laminate Configurations under Compression Diaconu, C., Weaver, P. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Postbuckling Behaviour and Design of Laminated Composite Structures Using Reissner-Mindlin-Von Karman Type Plate Model Kere, P., Lyly, M., Koski, J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Solutions for morphing airfoil sections using bi-stable laminated composite structures C. Diaconu, P. Weaver, F. Mattioni American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Approximate Solution for the Compression Buckling of Fully-Anisotropic Cylindrical Shells Wong, K., Weaver, P. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Optimal Design of Laminated Composite Plate for Maximum Postbuckling Strength Seresta, O., Abdalla, M., Gurdal, Z. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Design Formulae for Buckling of Biaxially Loaded Laminated Rectangular Plates with Flexural/twist Anisotropy Weaver, P. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Postbuckling and Growth of Delaminations in Composite Plates Subjected to Axial Compression Reeder, J., Song, K., Chunchu, P., Ambur, D. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Improved Design Formulae for Buckling of Orthotropic Plates Under Combined Loading P. Weaver, M. Nemeth American Institute of Aeronautics and Astronautics
5 テクニカルペーパー On Optimisation of Long Anisotropic Flat Plates Subject to Shear Buckling Loads Weaver, P. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Nonlinear Damped Vibrations of a Laminated Composite Plate Subject to Blast Load Kazanci, Z., Mecitoglu, Z. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Buckling and Postbuckling Behavior of Laminated Composite Plates With a Cutout Nemeth, Michael P. National Aeronautics and Space Adminstration	12 テクニカルペーパー MECHANICAL RESPONSE OF THICK LAMINATED BEAMS AND PLATES SUBJECT TO OUT-OF-PLANE LOADING Hiel, C. C. et al. National Aeronautics and Space Administration

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