A Finite Element Analysis Based on Higher-order Zig-zag Shell Theory for Laminated Composites with Multiple Delaminations

A Finite Element Analysis Based on Higher-order Zig-zag Shell Theory for Laminated Composites with Multiple Delaminations

著者名:

Oh, J. ( Seoul National University, Seoul, South Korea )
Cho, M.
Kim, J. ( Pennsylvania State University, University Park, PA )

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:

2004-2006

ペーパー番号:

AIAA-2004-2006

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 Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag Theory Cho, M., Oh, J., Kim, J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Shape and Layup Optimization of Laminated Composite Shells Based on Integrated Framework of Modeling and Analysis Cho, M., Kim, H., Roh, H. American Institute of Aeronautics and Astronautics
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