[1] Bradley W.L, Cohen R.N, (1985), "Matrix deformation and fracture in graphite-reinforced epoxies, Delamination and Debonding of Materials", American Society for Testing and Materials, Philadelphia, ASTM STP 876, 389-410.
[2] Davies P, Blackman B.R.K, Brunner A.J, (1998), "Standard test methods for delamination resistance of composite materials: current status". Appl Compos Mater, 5(6), 345–64.
[3] Xiao F., Hui C.-Y, Kramer E.J, (1993), "Analysis of a mixed mode fracture specimen: the asymmetric double cantilever beam", Journal of Materials Science, 28, 5620-562.
[4] ASTM D5528, (2007), "Standard test method for mode I interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites". Annual book of ASTM standards,15,1-12.
[5] Sriharan.S, (2008), "Delamination Behavior of composite" ,Published by Woodhead Publishing and Maney Publishing on behalf of The Institute of materials, Mainerals & Mining, CRC Press Boca Raton Boston New York Washington.
[6] Sheinman I, Kardomateas G.A, (1997), "Energy release rate and stress intensity factors for delaminated composite laminates". Int J Solids Struct, 34(4), 451–9.
[7] Sela N, Ishai O, (1989), "Interlaminar fracture toughness and toughening of laminated composite materials", a review.Composites, 20(5), 416.
[8] Barrett J.D, Foschi R.O, (1977), "Mode II stress intensity factors for cracked wood beams", Engng Fract Mech, 9(3), 371–8.
[9] O’Brien T.K, (1982), "Characterization of delamination onset and growth in a composite laminate" .In: Reifsnider KL, editor. Damage in composite materials. American Society for Testing and Materials, ASTM STP 775, 140–67.
[10] Williams J.G, (1988), "On the calculation of energy release rates for cracked laminates", International Journal of Fracture, 36(2), 101–119.
[11] Creton C, Kramer E.J, Hui C.Y, Brown H.R, (1992), "Failure mechanisms of polymer interfaces reinforced with block copolymers", Macromolecules, 25, 3075–3088.
[12] Kanninen M.R, (1974), "A dynamic anaiysis of unstable crack propagation and arrest in the DCB test specimen", International Journal of Fracture, 10(3), 415-430.
[13] Kanninen M.F, (1973), "An augmented double cantilever beam model for studying crack propagation and arrest", Int. J. Fracture, 9(1), pp-83-92.
[14] Kondo K, (1995), "Analysis of double cantilever beam specimen", Adv. Composite Materials, 4(4), 355-366.
[15] Ozdil F, Carlsson L. A, (1999), "Beam analysis of angle-ply laminate DCB specimens", 0, 59, 305-315.
[16] Williams J.G, (1989(, "End Corrections for Orthotropic DCB Specimens", Composite Science and Technology, 35, 367-376.
[17] Whitney J.M, (1985), "Stress Analysis of the Double Cantilever Beam Specimen", Composite Science and Technology, 23, 201-219.
[18] Olsson R.A, (1992),"A simplified improved beam analysis of the DCB specimen", Composite Science and Technology, 43, 329-338.
[19] Shokrieh M.M, Heidari Rarani M, Ayatollahi M.R, (2011), "Calculation of GI for a multidirectional composite double cantilever beam on two-parametric elastic foundation", Aerosp Sci Technol, 15, 534-543.
[20] Gdoutos E.E, Pilakoutas K. Chris A. Rodopoulos, (2000), "Failure Analysis of Industrial Composite Materials", McGraw-Hill Professional, 553 pages.
[21] Krueger R, (2002), "The Virtual Crack Closure Technique: History, Approach and Applications", NASA/CR-211628.
[22] Shivakumar K.N, Tan P. W, Newman J. C, (1988), "A Virtual Crack Closure Technique for Calculating Stress Intensity Factors for Cracked Three-Dimensional Bodies", Int. J. Fract. 36, 43-50.
[23] Ducept F, Gamby D, Davies P, (1999), "A mixed-mode failure criterion derived from tests on symmetric and asymmetric specimens", 59, 609-619.
)