Dimensions and Laminates Optimization of hat-stiffened Composite Panel with Buckling Load Constraint using Multi-objective GA

Dimensions and Laminates Optimization of hat-stiffened Composite Panel with Buckling Load Constraint using Multi-objective GA

著者名:

A. Todoroki ( Tokyo Institute of Technology, Tokyo, Japan )
M. Sekishiro

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Infotech@Aerospace Conference and Exhibit

シリーズ巻号:

2007

発行年:

2007

通号:

2007-2880

ペーパー番号:

AIAA Paper 2007-2880

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200709 [CD-ROM 2007 Disc 9]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049497
シリーズID:	PA00000048
会議名:	AIAA Infotech@Aerospace Conference and Exhibit
回次:	2007
会議開催地:	Rohnert Park, California
会議開催年:	2007.05.07-2007.05.10

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6 テクニカルペーパー Shear Buckling Analysis of a Hat-Stiffened Panel Ko, William L., Jackson, Raymond H. National Aeronautics and Space Adminstration	12 テクニカルペーパー Estimation of buckling loads of laminated composite plates with flaws using a system identification approach Salunkhe, Anil L., Mujumdar, Prasanna M. American Institute of Aeronautics and Astronautics

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