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Fracture Tests on Thin Sheet 2024-T3 Aluminum Alloy for Specimens with and Without Anti-Buckling GuidesA series of fracture test were conducted to determine the effects of specimen type specimen width and buckling on the fracture behavior of cracked thin sheet (0.063 inch thick) 2024-T3 aluminum alloy. A summary of the experimental measurements is presented for fracture tests conducted on two specimen types and various widths. Middle-crack tension M(T) and compact tension C(T) specimens were tested in the L-T and T-L orientation with duplicate tests for each condition. Four widths (W= 3, 12, 24, and 40 inch) were tested for the middle-crack tension specimens, and three widths (W=2, 4, and 6 inch) were tested for the compact tension specimens. The M(T) specimens were tested in either a constrained (out-of-plane displacements restrained with antibuckling guides) or unconstrained conditions were the specimen was free to buckle out of plane Measurements were made of load against crack extension for all specimens.
Document ID
20010041345
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Johnston, William M.
(Analytical Services and Materials, Inc. Hampton, VA United States)
Newman, James C., Jr.
Date Acquired
September 7, 2013
Publication Date
March 1, 2001
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.26:210832
NASA/CR-2001-210832
Report Number: NAS 1.26:210832
Report Number: NASA/CR-2001-210832
Funding Number(s)
CONTRACT_GRANT: NAS1-96014
PROJECT: RTOP 706-61-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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