Plasticity Tool for Predicting Shear Nonlinearity of Unidirectional Laminates Under Multiaxial Loading

• Published in: NASA Center for AeroSpace Information (CASI). Conference Proceedings
• Main Authors: Wang, John T, Bomarito, Geoffrey F
• Format: Conference Proceeding
• Language: English
• Published: Hampton NASA/Langley Research Center 19.09.2016
• Subjects: Damage assessment; Finite element method; Laminates; Micromechanics; Model testing; Modulus of elasticity; Nonlinearity; Plastic properties; Shear stress; Stress-strain curves; Stress-strain relationships; Unidirectional composites

This study implements a plasticity tool to predict the nonlinear shear behavior of unidirectional composite laminates under multiaxial loadings, with an intent to further develop the tool for use in composite progressive damage analysis. The steps for developing the plasticity tool include establishing a general quadratic yield function, deriving the incremental elasto-plastic stress-strain relations using the yield function with associated flow rule, and integrating the elasto-plastic stress-strain relations with a modified Euler method and a substepping scheme. Micromechanics analyses are performed to obtain normal and shear stress-strain curves that are used in determining the plasticity parameters of the yield function. By analyzing a micromechanics model, a virtual testing approach is used to replace costly experimental tests for obtaining stress-strain responses of composites under various loadings. The predicted elastic moduli and Poisson's ratios are in good agreement with experimental data. The substepping scheme for integrating the elasto-plastic stress-strain relations is suitable for working with displacement-based finite element codes. An illustration problem is solved to show that the plasticity tool can predict the nonlinear shear behavior for a unidirectional laminate subjected to multiaxial loadings.