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Analysis and Test of Deep Flaws in Thin Sheets of Aluminum and Titanium. Volume 1: Program Summary and Data AnalysisSix thicknesses of 2219-T87 aluminum base metal surface flaw and center crack specimens ranging from 9.53 to 0.635 mm (0.375 to 0.025 inch) were tested at temperatures ranging from 295K to 20K. Additionally, 6A1-4V STA titanium base metal specimens were tested in three thicknesses 3.18, 2.03, and 1.02 mm (0.125, 0.080 and 0.040 inch) at room temperature. All tests were conducted on uniaxial specimens. Results were analyzed and compared with previously developed data to establish a criterion for proof testing thin walled pressure vessels. The data analysis and exact flaw size dimensions are presented.
Document ID
19780013550
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Finger, R. W.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-135369
D180-24613-1
Report Number: NASA-CR-135369
Report Number: D180-24613-1
Accession Number
78N21493
Funding Number(s)
CONTRACT_GRANT: NAS3-19697
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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