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Detection of tightly closed flaws by nondestructive testing (NDT) methods in steel and titaniumX-radiographic, liquid penetrant, ultrasonic, eddy current and magnetic particle testing techniques were optimized and applied to the evaluation of 4340 steel (180 KSI-UTS) and 6Al-4V titanium (STA) alloy specimens. Sixty steel specimens containing a total of 176 fatigue cracks and 60 titanium specimens containing a total of 135 fatigue cracks were evaluated. The cracks ranged in length from .043 cm (0.017 inch) to 1.02 cm (.400 inch) and in depth from .005 cm (.002 inch) to .239 cm (.094 inch) for steel specimens. Lengths ranged from .048 cm (0.019 inch) to 1.03 cm (.407 inch) and depths from 0.010 cm (.004 inch) to .261 cm (0.103 inch) for titanium specimens. Specimen thicknesses were nominally .152 cm (0.060 inch) and 0.635 cm (0.250 inch) and surface finishes were nominally 125 rms. Specimens were evaluated in the "as machined" surface condition, after etch surface and after proof loading in a randomized inspection sequence.
Document ID
19770008190
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rummel, W. D.
(Martin Marietta Aerospace Denver, CO, United States)
Rathke, R. A.
(Martin Marietta Aerospace Denver, CO, United States)
Todd, P. H., Jr.
(Martin Marietta Aerospace Denver, CO, United States)
Tedrow, T. L.
(Martin Marietta Aerospace Denver, CO, United States)
Mullen, S. J.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1976
Subject Category
Metallic Materials
Report/Patent Number
MCR-76-476
NASA-CR-151098
Report Number: MCR-76-476
Report Number: NASA-CR-151098
Accession Number
77N15133
Funding Number(s)
CONTRACT_GRANT: NAS9-14653
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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