NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of Crack-Tip Configurations on the Fracture Response of 0.04-Inch Thick 2024-T3 Aluminum Alloy SheetA series of fracture tests were conducted on Middle-crack tension M(T) and compact tension C(T) specimens to determine the effects of specimen type, specimen width, notch tip sharpness and buckling on the fracture behavior of cracked thin sheet (0.04 inch thick) 2024-T3 aluminum alloy material. A series of M(T) specimens were tested with three notch tip configurations: (1) a fatigue pre-cracked notch, (2) a 0.010-inch-diameter wire electrical discharge machined (EDM) notch, and (3) a EDM notch sharpened with a razor blade. The test procedures are discussed and the experimental results for failure stress, load vs. crack extension and the material stress-strain response are reported.
Document ID
20020029619
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Johnston, William M.
(Analytic Services and Materials, Inc. Hampton, VA United States)
Newman, James C.
Date Acquired
September 7, 2013
Publication Date
February 1, 2002
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/CR-2002-211442
NAS 1.26:211442
Report Number: NASA/CR-2002-211442
Report Number: NAS 1.26:211442
Funding Number(s)
PROJECT: RTOP 706-61-11-03
CONTRACT_GRANT: NAS1-96014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available