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Nicolas Krumenacker and Pascal Hubert [6] C. Ridgard, Out of autoclave composite technology for aerospace, defense and space structures, Proceedings of the SAMPE 2010 Spring Symposium (Eds. J.C. Fielding, S. Prybyla, L. Tate and S.W. Beckwith), Baltimore, MD, USA, May 18-21, 2009, SAMPE, Covina, 2009, Paper 218, pp. 1-11. [7] S. Mortimer and M.J. Smith, Product development for out-of-autoclave (O.O.A.) manufacture of aerospace structure, Proceedings of the SAMPE 2010 Spring Symposium & Exhibition (Eds. R. Albers, P. Hubert and S.W. Beckwith), Seattle, WA, United States, May 17-20, 2010, SAMPE, Covina, 2010, Paper 379, pp. 1-11. [8] C. Ridgard, Next generation out of autoclave systems, Proceedings of the SAMPE 2010 Spring Symposium & Exhibition (Eds. R. Albers, P. Hubert and S.W. Beckwith), Seattle, WA, United States, May 17-20, 2010, SAMPE, Covina, 2010, Paper 180, pp. 1-18. [9] R. 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[24] ASTM standard D6415, 2006a (2013), Standard test method for measuring the curved beam strength of a fiber-reinforced polymer-matrix composite, ASTM International, 100 Bar Harbor Drive, West Conshohocken, PA 19428, United States, 2014 (doi: 10.1520/D6415_D6415M). [25] J. Kratz, K. Hsiao, G. Fernlund and P. Hubert, Thermal models for MTM45-1 and Cycom 5320 out-of- autoclave prepreg resins, Journal of Composite Materials, 47, 2013, pp. 341-352 (doi: 10.1177/0021998312440131). [26] G. Seon, A. Makeev, Y. Nikishkov and E. Lee, Effects of defects on interlaminar tensile fatigue behavior of carbon/epoxy composites, Composites Science and Technology, 89, 2013, pp. 194-201 (doi: 10.1016/j.compscitech.2013.10.006).PDF Image | VACUUM-BAG-ONLY COMPLEX-SHAPE PREPREG LAMINATE
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