NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Impact and Penetration Simulations for Composite Wing-like StructuresThe goal of this research project was to develop methodologies for the analysis of wing-like structures subjected to impact loadings. Low-speed impact causing either no damage or only minimal damage and high-speed impact causing severe laminate damage and possible penetration of the structure were to be considered during this research effort. To address this goal, an assessment of current analytical tools for impact analysis was performed. Assessment of the analytical tools for impact and penetration simulations with regard to accuracy, modeling, and damage modeling was considered as well as robustness, efficient, and usage in a wing design environment. Following a qualitative assessment, selected quantitative evaluations will be performed using the leading simulation tools. Based on this assessment, future research thrusts for impact and penetration simulation of composite wing-like structures were identified.
Document ID
19980017259
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Knight, Norman F.
(Old Dominion Coll. Norfolk, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 30, 1998
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:206825
NASA/CR-1998-206825
Report Number: NAS 1.26:206825
Report Number: NASA/CR-1998-206825
Funding Number(s)
CONTRACT_GRANT: NAG1-1858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available