OPTIMIZING MATERIAL STRENGTH CONSTANTS NUMERICALLY EXTRACTED FROM TAYLOR IMPACT DATA

Advanced design requirements have dictated a need for the mechanical p roperties of materials at high strain rates. Mechanical testing for th ese data poses a significant problem for experimentalists. High-speed testing machines have a limited capability at rates approaching 10(2)/ s. The split Hopkinson pressure bar is the most reliable alternative f or rates approaching 10(4)/s. Plate impact experiments are capable of generating strain rates of 10(8)/s and higher, The Taylor impact test occupies a place of particular importance by providing data at strain rates on the order of 10(4)/s-10(5)/s. The issue at present is extract ing the data, This paper provides a method for obtaining dynamic stren gth model material constants from a single Taylor impact test. A polyn omial response surface is used to describe the volume difference (erro r) between the deformed specimen from the Taylor test and the results of a computer simulation. The volume difference can be minimized using an optimizer, with the result being an optimum set of material consta nts, This method was applied to the modified Johnson-Cook model for OF HC copper, Starting from a nominal set of material constants, the iter ative process improved the relative volume difference from 23.1 percen t to 4.5 percent. Other starting points were used that yielded similar results, The material constants were validated by comparing numerical results with Taylor tests of cylinders having varying aspect ratios, calibers and impact velocities.