LRIR Proposal- An Efficient Solution Method for Large-Scale Progressive Fracture Simulations of Advanced Composite Materials

Abstract

Multiscale methods have enabled many successes in capturing the multiscale nature of composite materials. However, nearly all such approaches rely on a periodic unit-cell that can be mathematically leveraged to make the simulations tractable. This project aims to develop a novel solution method that focuses on both the multiscale nature of composites and a solver that enables the direct simulation of fracture across length scales for complex composite components. We hold that a solution method that leverages both grid coarsening and model coarsening, that is, physics models designed for different length scales, can circumvent the limitations of multigrid methods and converge faster than general-purpose solvers for large simulations. The proposed work will open a new frontier of integrated computational materials engineering (ICME) by enabling component-level performance simulations that directly consider the micro-mesoscale.

Document Details

Document Type
DoD Grant Award
Publication Date
Feb 06, 2025
Source ID
FA95502510042

Entities

People

  • Varun Shankar

Organizations

  • Air Force Office of Scientific Research
  • United States Air Force
  • University of Utah

Tags

Readers

  • Computational Fluid Dynamics (CFD)
  • Reinforced Composite Materials