OPTIMUM LAYUP OF THICK LAMINATED COMPOSITE PLATES FOR MAXIMUM STIFFNESS-Reference-Cited by-同舟云学术

OPTIMUM LAYUP OF THICK LAMINATED COMPOSITE PLATES FOR MAXIMUM STIFFNESS

Published:1992-05 Issue:3 Volume:19 Page:237-249
ISSN:0305-215X
Container-title:Engineering Optimization
language:en
Short-container-title:Engineering Optimization

Author:

KAM T. Y.,CHANG R. R.

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Link

http://www.tandfonline.com/doi/pdf/10.1080/03052159208941230

Reference28 articles.

1. Stroud , W. J. and Agranoff , N. ( 1976 ) Minimum-mass design of filamentary composite panels under combined load Design procedure based on simplified buckling equations , NASA TN D-8257 , NASA Langley Research Center , Hampton , VA .

2. Optimum design of laminated fibre composite plates

3. Computer Sizing of Composite Laminates for Strength

4. Multilevel optimal design of laminated composite plate structures

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