Residual stresses and the optimum cure cycle for an epoxy resin-Reference-Cited by-同舟云学术

Residual stresses and the optimum cure cycle for an epoxy resin

Published:1989-06 Issue:6 Volume:24 Page:1984-1990
ISSN:0022-2461
Container-title:Journal of Materials Science
language:en
Short-container-title:J Mater Sci

Author:

Hodges J.,Yates B.,Darby M. I.,Wostenholm G. H.,Clemmet J. F.,Keates T. F.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/BF02385410.pdf

Reference9 articles.

1. B. YATES, B. A. McCALLA, L. N. PHILLIPS, D. M., KINGSTON-LEE and K. F. ROGERS,J. Mater. Sci. 14 (1979) 1207.

2. J. F. CLEMMET, Typical Examples of European Technology for High Stability Space Structures, AGARD—Requirements, Design and Development of Large Space Antenna Structures, May, 1980.

3. J. F. CLEMMET,Aerospace Dynamics September (1982) 25.

4. C. C. CHAMIS, “Lamination Residual Stresses in Cross-Plied Fibre Composites”, NASA-TM-X-52881 (1971).

5. P. L. SANDALLS, PhD thesis, University of Salford (1983).

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