SYMPOSIA PAPER Published: 01 January 1975

Toughness Variations Through the Thickness of Thick 5083-0 Aluminum Alloy Plate


Dynamic tear tests at the Naval Research Laboratory (NRL), using a series of beam specimens with increasing depth, have shown that the toughness of 3-in.-thick 5083 plate varied from surface to mid-plane. To explore the possible extent of such variation in still thicker plate and provide an economical test for assessing the effect of process variables on toughness, similar specimens were tested under static loading.

The data obtained could be interpreted with the aid of the plastic resistance concept used by NRL. We found that they would also yield approximate values of strain energy release rate at crack initiation (GIc), thus, linking the dynamic tear test and ratio analysis diagram directly to elastic-plastic fracture mechanics. The test method is much more economical than full plate thickness tests, and the results are believed to be more indicative of the materials' resistance to fracture than small specimen (invalid) KIc values, which are more indicative of material yield strength and the crack length dictated by specimen size, than they are of toughness.

Surface layers of one 5083-0 plate, 7.75 in. thick (195 mm), were found to be 20 to 30 percent tougher than center layers at room temperature. Toughness of the surface layers improved somewhat as the temperature was lowered to -260°F (-162°C). However, the improvement of the center layers was more dramatic. At the lower test temperature toughness was essentially uniform throughout the plate thickness.

Author Information

Lake, RL
Kaiser Aluminum and Chemical Corporation, Center for Technology, Pleasanton, Calif.
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Developed by Committee: E50
Pages: 176–189
DOI: 10.1520/STP29161S
ISBN-EB: 978-0-8031-4659-4
ISBN-13: 978-0-8031-0538-6