By John S. Rinehart (auth.), Marc A. Meyers, Lawrence E. Murr (eds.)
The clinical figuring out of high-velocity deformation has complicated considerably in the past decade. at the one hand, the framework for a thought explaining the metallurgical results of outrage waves is starting to take form; nonetheless, the technological purposes of excessive strain-rate tactics have came across their method into industries in international locations world wide. Ex plosive cladding, welding, forming, compaction and consolidation, slicing, and hardening, as well as excessive energy-rate deformation approaches utilizing different power resources, are a number of the themes of up to date technological value. Metallurgical results are of the maximum value in either the clinical knowing of the phenomena concerned, and within the winning improvement and usage of the linked purposes. The foreign convention upon which this ebook relies had as its significant targets the acceleration of development within the box of high-strain cost deformation and fabrication, together with purposes, through delivering a discussion board for the alternate of state-of-the artwork info at the metallurgical results of excessive strain-rate deformation and fabrication; and the association of this informa tion right into a well timed and coherent physique of data concentrated round major parts and functions. This quantity is a manifestation of those pursuits. additionally, the contents of this publication have been geared up to supply for a a little logical viewpoint of the basics, improvement, and state of the art purposes of excessive strain-rate and surprise phenomena.
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Interscience, New York, 1960. , Hugoniot Equation of State of Aluminum and Steel From Oblique Measurements, J. AppZ. , :30, 568, (1959). , The Hugoniot Equation of State of 6061-T6 Aluminum at Low Pressures, SC-4637 (RR). 19 p. , Albuquerque, 1961. , Propagation of Shock Waves in Aluminum. J. AppZ. , 26, 555, (1955). G. , Equation of State of Nineteen Metallic Elements From Shock Wave Measurements to two Megabars, J. AppZ. , :31, 1253, (1960). , Residual Temperatures of Shock Loaded Iron, in "Proc.
E. CARDEN ET AL. 42 much scatter in replicate tests (at 10- 3 S-l we performed seven replicate tests) as there is between the flow curves at different strain rates. At least two tests were performed at each strain rate. , chemistry of the original ingot) and product form (sheet vs plate) were different for the tensile and expanding ring specimens. The tensile test data, therefore, are most valuable for determining if there are strainrate effects at the low strain rates. The absolute value of the flow stress may be different for the ring and tensile specimens at the same strain rate.
DJ FIGURE 5. Comparison of ring velocities for nominally-identical experiments: (aJ strongly-loaded annealed copper; (bJ moderately-loaded annealed copper; (cJ strongly-loaded hardened copper; (dJ moderately-loaded hardened copper. EXPANDING RING TECHNIQUE 33 continues to strain. until a pOint is reached when the data become oscillatory and of questionable validity. Data are only considered during the smooth. midrange of travel. Note that early-time agreement of the two velocity-time traces is quite impressive.