Explicit Finite Element Modeling of Multilayer Composite Fabric for Gas Turbine Engine Containment Systems, Phase II. Part 1: Fabric Material Tests and Modeling

摘要

Under the Federal Aviation Administration Airworthiness Assurance Center of Excellence, sponsored by the Aircraft Catastrophic Failure Prevention Program, a research team consisting of members from Arizona State University (ASU), Honeywell Engines, Systems & Services (Honeywell), National Aeronautics and Space Administration Glenn Research Center (NASA-GRC), and SRI International (SRI) collaborated to develop test procedures and computational models for designing and evaluating ballistic fabric containment structures. This report contains the details of additional tensile tests, friction tests, and static ring tests and their finite element simulations conducted at ASU. It also contains a comparison of the Honeywell and SRI finite element models of the NASA-GRC ballistic impact tests.