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Shear strength of fillet welds in aluminum alloy 2219Fillet size is discussed in terms of theoretical or design dimensions versus as-welded dimensions, drawing attention to the inherent conservatism in the design load sustaining capabilities of fillet welds. Emphasis is placed on components for the solid rocket motor, external tank, and other aerospace applications. Problems associated with inspection of fillet welds are addresses and a comparison is drawn between defect counts obtained by radiographic inspection and by visual examination of the fracture plane. Fillet weld quality is related linearly to ultimate shear strength. Correlation coefficients are obtained by simple straight line regression analysis between the variables of ultimate shear strength and accumulative discontinuity summation. Shear strength allowables are found to be equivalent to 57 percent of butt weld A allowables (F sub tu.)
Document ID
19780013552
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lovoy, C. V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-78168
Report Number: NASA-TM-78168
Accession Number
78N21495
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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