NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Analysis of delamination in fiber composite laminates out-of-plane under bendingDelamination in the form of cracking or separation between plies in an advanced fiber composite laminate is a problem of major concern. Both advanced analytical methods and advanced computational analyses are conducted to: (1) develop an asymptotic solution for a composite laminate subject to out-of-plane bending; (2) construct advanced singular finite elements in conjunction with the development of nonsingular elements for this bending problem; and (3) evaluate the delamination failure mechanics parameters and the subsequent modes of fracture. A parametric study was also conducted to evaluate the influences of various lamination parameters on the delaminated composites.
Document ID
19910000809
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wang, S. S.
(Illinois Univ. Urbana, IL, United States)
Yuan, F. G.
(Illinois Univ. Urbana, IL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:186923
NASA-CR-186923
Report Number: NAS 1.26:186923
Report Number: NASA-CR-186923
Accession Number
91N10122
Funding Number(s)
CONTRACT_GRANT: NAG1-286
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available