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AMTAS is a consortium of academic institutions, aerospace companies, and government agencies. AMTAS seeks solutions to problems associated with existing, near- and long-term applications of composites and advanced materials for large transport commercial aircraft.

Publication Type: Conference Proceeding

Stochastic computational modeling of the fracturing behavior in discontinuous fiber composite structures

Experimental and numerical investigations of stochastic thickness effects in discontinuous fiber composites

Implicit versus Explicit Approaches to FEA Modeling of Notched Composite Panels

Mesh Dependency in Progressive Failure Modeling of Notched Laminates Under Out-of-Plane Bending

Mesh Selection for Modeling Progressive Damage in Mode III Shear for Composite Fiber Panels

Improvement on the Analysis of a Finite Element Composites Model

Effective Finite Element Modeling of Mode III Failure in Composites

Mesh Selection for Progressive Failure Modeling of Carbon Fiber Panels in Mode III Shear using an Explicit Finite Element Solver

Effects of Finite Element Damage Modeling Parameters in Carbon Fiber Panels Under Mode III Loading

Effects of Layup and Matrix Toughness on Modeling Notched Carbon Fiber Panels in Out-of-Plane Bending

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