참고문헌
- Ritchie, R.O., Yu, Weikang, and Bucci, R.J., 1989, 'Fatigue Crack Propagation in ARALL Laminates: Measurement of the Effect of Crack-Tip Shielding from Crack Bridging,' Engineering Fracture Mechanics, Vol. 32, No.3, pp. 361-377 https://doi.org/10.1016/0013-7944(89)90309-3
- Asundi, A. and Choi, Alta Y.N., 1997 'Fiber Metal Laminates:An Advanced Material for Future Aircraft,' Journal of Materials Processing Technology, Vol. 63, pp. 384-394 https://doi.org/10.1016/S0924-0136(96)02652-0
- Yeh, J.R., 1988, 'Fracture Mechanics of Delamination in ARALL Laminates,' Engineering Fracture Mechanics, Vol. 30, No.6, pp. 827-837 https://doi.org/10.1016/0013-7944(88)90144-0
- Macheret, J., Teply, J.L., and Winter, E.F.M., 1989, 'Delamination Shape Effects in Aramid-Epoxy-Aluminum (ARALL) Laminates With Fatigue Cracks:' Polymer Composites, Vol. 10, No.5, pp. 322-327 https://doi.org/10.1002/pc.750100508
- Sun, C.T. , Dicken, A., and Wu, H.F., 1993,. Characterization of Impact Damage in ARALL Laminates,' Composites Science and Technology, Vol 49, pp. 139-144 https://doi.org/10.1016/0266-3538(93)90053-J
- Vlot, A., 1996, 'Impact Loading on Fiber Metal Laminates,' Int. J. Impact Engineering, Vol. 18, No.3. pp.291-307 https://doi.org/10.1016/0734-743X(96)89050-6
- Lawcock, G.D., et al., 1997, 'Effects of Fiber/Matrix Adhesion on Carbon Fiber Reinforced Metal Larninates-II. Impact Behavior,' Composites Science and Technology. Vol. 57, pp. 1621-1628 https://doi.org/10.1016/S0266-3538(97)00094-8
- Lawcock, Glyn et al, 1997, 'Progressive Damage and Residual Strength of a Carbon Fiber Reinforced Metal Laminate,' J. of Composite Materials, Vol. 31. No.8, pp. 762-787 https://doi.org/10.1177/002199839703100802
- Zhi-He Jin and Yiu-Wing Mai, 1997, 'Residual Strength of an ARALL Laminate Containing a Crack,' J. of Composite Materials, Vol. 31, No.8, pp. 746-761 https://doi.org/10.1177/002199839703100801
- Lawcock, G.D. et al., 1997, 'Effects of Fiber/Matrix Adhesion on Carbon Fiber Reinforced Metal Laminates-I. Residual Strength,' Composites Science and Technology, Vol. 57, pp. 1609-1619 https://doi.org/10.1016/S0266-3538(97)00108-5
- Nuismer, R.J. and Whitney, J.M., 1975, 'Uniaxial Failure of Composite Laminate Containing Stress Concentrations.' In Fracture Mechanics of Composites, ASTM STP 593, American Society of Testing and Materials, pp. 117-142
- Peterson, R.E., 1974, Stress Concentration Factor, John Wiley & Sons, New York
- Lekhnitskii, S.G., 1968 Anisotropic Plates. Translated from the Second Russian Edition by S.W. Tsai and T. Cheron, Gordon and Breach. Science Piblishers, Inc .. New York
- Brown. W.F. Jr. and Srawley, John E.. 1966. 'Plane Strain Crack Toughness Testing of High Strength Metallic Materials,' ASTM STP 410, American Society for Testing and Materials
- Mar, J. 1976. 'Fracture and Fatigue in Bi-Materials.' in Mechanics of Composite Review, Air Force Materials Laboratory and Air Force Office of Scientific Research Technical Report, pp. 117-122
- Nam, H.W. Kim, Y.H. and Han. K.S., 2001. 'Damage Analysis of Fiber Metal Laminates using Acoustic Emission.' KSCM Journal. Vol. 14. No.5, pp.42-50
- Wegman. Raymond F., 1989, Surface Preparation Techniques for Adhesive Bonding, Noyes Publications
- Trawinski, D., 1984, 'A Low Temperature Etchant Surface Preparation for Steel Adhesive Bonding,' SAMPE Quarterly, Vol. 16. No. 1. Oct., pp. 1-5
- Hitchcn, S.A and Kemp. R.M.J., 1995 'Effect of Stacking Sequence on Impact Damage,' Composites, Vol. 26. No.2. pp. 154-160 https://doi.org/10.1016/0010-4361(95)91384-H