Page 234 - 3D Fibre Reinforced Polymer Composites
P. 234
References 223
Dransfield K.A., L.K. Jain and Y.-W. Mai, 1998, On the effects of stitching in CFRPs -
I. Mode I delamination toughness, Comp. Sci. & Tech., 58:815.
Du X., F. Xue and 2. Gu, 1986, Experimental study of the effect of stitching on strength
of a composite laminate, Proc. Int. Symp. Comp. Mat. & Struct., 10-13 Jun., 912-
918.
Editor 1996, Total garment technology - the pursuit of WholeGarment production,
Knitting Int., DecembedJanuary.
Editor 1997, Flat frame machines, Knitting Int., March, 30-31.
Emehel T.C. and K.N. Shivakumar, 1997, Tow collapse model for compression strength
of textile composites, J. Rein. Plastics & Comp., 16:86-101.
Epstein M. and S. Nurmi, 1991, Near net shape knitting of fiber glass and carbon for
composites, Proc. of the 36" Int. SAMPE Symposium, April 15-18,102-113.
Evans D. and J. Boyce, 1989, Transverse reinforcement methods for improved
delamination resistance, 34'h Int. SAMPE Symposium, May 8-1 1,271-282.
Farley G.L., 1992, A mechanism responsible for reducing compression strength of
through-the-thickness reinforced composite material, J. Comp. Mat., 26: 1784.
Farley G., 1993, Method and apparatus for weaving a woven angle ply fabric, US Patent
5,224,519,6 July.
Farley G.L. and Dickinson, L.C., 1992, Removal of surface loop from stitched
composites can improve compression and compression-after-impact strengths, J.
Rein. Plast. & Comp., 11:633.
Farley G.L., B.T. Smith and J. Maiden, 1992, Compression response of thick layer
composite laminates with through-the-thickness reinforcement, J. Rein. Plast. &
Comp., 11:787-810.
Fedro M.J. and K. Willden, 1991, 'Characterization and manufacture of braided
composites for large commercial aircraft structures', NASA CP 3 154, Second NASA
Advanced Composites Technology Conf., 4-7 Nov., 387-429.
Filatovs G.J., R. L. Sadler and A. El-Shiekh, 1994, Fracture-behavior of a 3-d braid
graphite-epoxy composite, J. Comp. Mat., 28526-542.
Florentine R., 1982, Apparatus for weaving a three-dimensional article, US Patent
4,312,261, January 26.
Freitas G. and M. Dubberly, 1997, Joining aluminium materials using ultrasonic
impactors, J. Metals, May, 3 1.
Freitas G., T. Frusco, T. Campbell, J. Harris and S. Rosenberg, 1996, Z-Fiber
technology and products for enhancing composite design, Proc. of the 83'' Meeting
of the AGARD SMP on "BoltedKionded Joints in Polymeric Composites", Sep. 2-3,
Florence, Italy, pp.17-1 - 17-8.
Freitas G., C. Magee, P. Dardzinski and T. Fusco, 1994, Fiber insertion process for
improved damage tolerance in aircraft laminates, J. Advanced Mat., 25:36-43.
Freitas G., C. Magee, J. Boyce and R. Bott, 1991, Service tough composite structures
using z-fiber process, Proc. 9" DoD/NASA/FAA Conf. Fibrous Comp., Lake Tahoe,
Nevada, Nov.
Fukuta K., Y. Nagatsuka, S. Tsuburaya, R. Miyashita, J. Sekiguti, E. Aoki and M.
Sasahara, 1974, Three-dimensional fabric and method and construction for the
production thereof, US Patent No. 3,834,424, Sep. 10.