NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Modeling and Characterization of Crushable Composite Structures The crushing response and the energy absorption capacity of a quasi-isotropic C-shaped composite panel is presented to simulate the progressive damage and failure mechanisms involved in the component testing. Crushable composite structures are widely used for impact applications, as because of their great high-energy absorption capability and lower weight. Simulating the crush characteristics of composite structures is challenging, as the conventional tools fail to accurately represent the failure mechanisms at the component level. Here, a cost-effective predictive tool ‘CZone’ is applied for simulating the crushing response of composite materials. CZone for Abaqus (CZA) is an add-on capability for Abaqus/Explicit and combines with the commercially available impact modeling capabilities included within the Abaqus finite element software package.
Document ID
20220018601
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Deepak K. Patel
(Dassault Sytems)
Evan J. Pineda
(Glenn Research Center Cleveland, Ohio, United States)
Paria Naghipour
(HX5, LLC)
Steven M. Arnold
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
December 7, 2022
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech Forum
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.03.05.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
crush zone
composite impact simulation
quasi-static crushing of composites
No Preview Available