A generalized multilength scale nonlinear composite plate theory with delamination

Abstract A new type of plate theory for the nonlinear analysis of laminated plates in the presence of delaminations and other history-dependent effects is presented. The formulation is based on a generalized two length scale displacement field obtained from a superposition of global and local displacement effects. The functional forms of global and local displacement fields are arbitrary. The theoretical framework introduces a unique coupling between the length scales and represents a novel two length scale or local-global approach to plate analysis. Appropriate specialization of the displacement field can be used to reduce the theory to any currently available, variationally derived, displacement based (discrete layer, smeared, or zig-zag) plate theory. The theory incorporates delamination and/or nonlinear elastic or inelastic interfacial behavior in a unified fashion through the use of interfacial constitutive (cohesive) relations. Arbitrary interfacial constitutive relations can be incorporated into the theory without the need for reformulation of the governing equations. The theory is sufficiently general that any material constitutive model can be implemented within the theoretical framework. The theory accounts for geometric nonlinearities to allow for the analysis of buckling behavior. The theory represents a comprehensive framework for developing any order and type of displacement based plate theory in the presence of delamination, buckling, and/or nonlinear material behavior as well as the interactions between these effects. The linear form of the theory is validated by comparison with exact solutions for the behavior of perfectly bonded and delaminated laminates in cylindrical bending. The theory shows excellent correlation with the exact solutions for both the inplane and out-of-plane effects and the displacement jumps due to delamination. The theory can accurately predict the through-the-thickness distributions of the transverse stresses without the need to integrate the pointwise equilibrium equations. The use of a low order of the general theory, i.e. use of both global and local displacement fields, reduces the computational expense compared to a purely discrete layer approach to the analysis of laminated plates without loss of accuracy. The increased efficiency, compared to a solely discrete layer theory, is due to the coupling introduced in the theory between the global and local displacement fields.

[1]  A. Needleman.  A Continuum Model for Void Nucleation by Inclusion Debonding , 1987 .

[2]  V. V. Bolotin.  Delaminations in composite structures: Its origin, buckling, growth and stability , 1996 .

[3]  R. Christensen,et al.  A High-Order Theory of Plate Deformation—Part 2: Laminated Plates , 1977 .

[4]  Marco Di Sciuva,et al.  Multilayered anisotropic plate models with continuous interlaminar stresses , 1992 .

[5]  B. Storȧkers.  NONLINEAR ASPECTS OF DELAMINATION IN STRUCTURAL MEMBERS , 1989 .

[6]  Jack Beuth,et al.  Separation of crack extension modes in orthotropic delamination models , 1996 .

[7]  K. H. Lee,et al.  An improved zig-zag model for the bending of laminated composite shells , 1990 .

[8]  David Kennedy,et al.  Effect of Interfacial Imperfection on Buckling and Bending Behavior of Composite Laminates , 1996 .

[9]  A. Needleman.  An analysis of decohesion along an imperfect interface , 1990 .

[10]  Hidenori Murakami,et al.  A high-order laminated plate theory with improved in-plane responses☆ , 1987 .

[11]  J. N. Reddy,et al.  A refined nonlinear theory of plates with transverse shear deformation , 1984 .

[12]  J. N. Reddy,et al.  A generalization of two-dimensional theories of laminated composite plates† , 1987 .

[13]  R. Christensen,et al.  A HIGH-ORDER THEORY OF PLATE DEFORMATION, PART 1: HOMOGENEOUS PLATES , 1977 .

[14]  Todd O. Williams,et al.  A dynamic model for laminated plates with delaminations , 1998 .

[15]  J. Aboudi,et al.  DYNAMIC INELASTIC RESPONSE AND BUCKLING OF METAL MATRIX COMPOSITE INFINITELY WIDE PLATES DUE TO THERMAL SHOCKS , 1995 .

[16]  Hidenori Murakami,et al.  Laminated Composite Plate Theory With Improved In-Plane Responses , 1986 .

[17]  J. Aboudi,et al.  Dynamic buckling of metal matrix composite plates and shells under cylindrical bending , 1994 .

[18]  Alberto Corigliano,et al.  Formulation, identification and use of interface models in the numerical analysis of composite delamination , 1993 .

[19]  J. Whitney.  Structural Analysis of Laminated Anisotropic Plates , 1987 .

[20]  Maenghyo Cho,et al.  Efficient higher order composite plate theory for general lamination configurations , 1993 .

[21]  R. C. Averill,et al.  Thick beam theory and finite element model with zig-zag sublaminate approximations , 1996 .

[22]  Todd O. Williams,et al.  A general theory for laminated plates with delaminations , 1997 .

[23]  N. Pagano,et al.  Exact Solutions for Composite Laminates in Cylindrical Bending , 1969 .

[24]  Marco Di Sciuva,et al.  Development of an anisotropic, multilayered, shear-deformable rectangular plate element , 1985 .

[25]  Lan Xu,et al.  Stress analysis of imperfect composite laminates with an interlaminar bonding theory , 1994 .

[26]  S. Arnold,et al.  Thermoplstic response of metal-matrix composites with homogenized and functionally graded interfaces , 1994 .

[27]  M. D. Sciuva,et al.  BENDING, VIBRATION AND BUCKLING OF SIMPLY SUPPORTED THICK MULTILAYERED ORTHOTROPIC PLATES: AN EVALUATION OF A NEW DISPLACEMENT MODEL , 1986 .