NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Simulation Tool for Damage in Composite LaminatesA numerical simulation tool for progressive failure in laminates utilizes a low fidelity approach. The numerical model includes an enriched element that is initially in a low fidelity form. The enriched elements may increase fidelity by splitting locally to simulate an ongoing damage process such as delamination.
Document ID
20180004385
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
McElroy, Mark W.
Date Acquired
August 10, 2018
Publication Date
July 31, 2018
Subject Category
Quality Assurance And Reliability
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-10,036,700
Patent Application
US-Patent-Appl-SN-15/526,369
No Preview Available