NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance of a quantitative study of instability-related delamination growthAn experimental program was conducted to quantify instability-induced imbedded delamination growth. Static tests on double cantilever beam (DCB) specimens yielded the critical mode 1 strain energy release rate (G sub 1 C) for T300/5208 graphite/epoxy. Static tests on mixed mode cracked lap shear (CLS) specimens, and a nonlinear finite element analysis (NFEA) of the CLS specimen to separate mode 1 and mode 2 effects, yielded the critical mode 2 strain energy release rate (G sub 2 C) for T300/5208. Constant amplitude fatigue tests on DCB and CLS specimens, along with the NFEA results on CLS specimens, quantified mode 1 and mode 2 contributions to delamination growth rate. Fatigue tests were conducted at a frequency (omega) of 10 Hertz, maintaining the minimum to maximum cyclic load ratio (R) at 0.05. Static compression and constant amplitude compression fatigue tests were also conducted on specimens with imbedded through the width (ITTW) delaminations. Kapton imbeddments were located below 3, 4 or 6 plies in a 64-ply laminate, during layup, to simulate ITTW delaminations.
Document ID
19830021043
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ramkumar, R. L.
(Northrop Corp. Hawthorne, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Composite Materials
Report/Patent Number
NOR-83-70
NAS 1.26:166046
NASA-CR-166046
Report Number: NOR-83-70
Report Number: NAS 1.26:166046
Report Number: NASA-CR-166046
Accession Number
83N29314
Funding Number(s)
CONTRACT_GRANT: NAS1-16727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available