NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of Reinforcement Architecture on Fracture of Selectively Reinforced Metallic Compact Tension SpecimensA computer-based parametric study of the effect of reinforcement architectures on fracture response of aluminum compact-tension (CT) specimens is performed. Eleven different reinforcement architectures consisting of rectangular and triangular cross-section reinforcements were evaluated. Reinforced specimens produced between 13 and 28 percent higher fracture load than achieved with the non-reinforced case. Reinforcements with blunt leading edges (rectangular reinforcements) exhibited superior performance relative to the triangular reinforcements with sharp leading edges. Relative to the rectangular reinforcements, the most important architectural feature was reinforcement thickness. At failure, the reinforcements carried between 58 and 85 percent of the load applied to the specimen, suggesting that there is considerable load transfer between the base material and the reinforcement.
Document ID
20060009470
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Abada, Christopher H.
(National Inst. of Aerospace Hampton, VA, United States)
Farley, Gary L.
(Army Research Lab. Hampton, VA, United States)
Hyer, Michael W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 2006
Subject Category
Structural Mechanics
Report/Patent Number
L-19238
ARL-TR-3769
NASA/TM-2006-214286
Funding Number(s)
OTHER: 759.07.11
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available