Stability of graphite/epoxy structures with arbitrary symmetrical laminates

Author:

Spier Edward E.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference7 articles.

1. Spier, E.E. and Klouman, F.L., “Empirical Crippling Analysis of Graphite/Epoxy Laminated Plates,” Composite Materials: Testing and Design (4th Conf.), ASTM,ASTM STP 617 (1977).

2. Spier, E.E. and Klouman, F.L., “Post Buckling Behavior of Graphite/Epoxy Laminated Plates and Channels,” Proc. Army Symp. Solid Mechanics, 1976—Composite Materials: The Influence of Mechanics of Failure on Design, Army Materials and Mechanics Research Center, Watertown, MA,AMMRC MS 76-2 (Sept. 1976).

3. Spier, E.E. and Klouman, F.L., “Ultimate Compressive Strength and Nonlinear Stress-Strain Curves of Graphite/Epoxy Laminates,” Proc. 8th Natl. SAMPE Conf., “Bicentennial of Materials Progress—Part II”, Seattle, WA (Oct. 1976).

4. May, C.L., “Fabrication Methods for Graphite/Epoxy Tubular Structures,” unpublished.

5. Advanced Composites Design Guide, Vol. II—Analysis, Air Force Materials Lab., Advanced Development Division, Dayton, OH, Table 2.2.2-I (Jan. 1973).

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