Optimum design of laminated fibre composite plates-Reference-Cited by-同舟云学术

Optimum design of laminated fibre composite plates

Published:1977 Issue:4 Volume:11 Page:623-640
ISSN:0029-5981
Container-title:International Journal for Numerical Methods in Engineering
language:en
Short-container-title:Int. J. Numer. Meth. Engng.

Author:

Schmit L. A.,Farshi B.

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference7 articles.

1. Optimum laminate design for strength and stiffness

2. ‘Stiffness, strength and stability optimization of laminated composites’, Report NOR-70-138, Northrop Aircraft Corp., Hawthorne, California (1970).

3. and , ‘Strength and stability optimization of an unstiffened panel under multiple inplane loads’, Chapter 1.8, Advanced Composites Design Guide, 3rd edn, AFML, WPAFB, Ohio (1973).

4. Sandwich Construction for Aircraft, ANC 23, Pt. II, 2nd edn, U.S. Government Printing Office, Wash., D.C., 1955.

5. ‘Stability analysis of advanced filamentary composite panels’, Report TR-AC-SM-8087, Grumman Aerospace Corp., Bethpage, New York (1970).

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