This technique compares a random pattern on the surface of an object before and after the object is deformed to investigate the amount of pattern movement. The random pattern used here was printed on a transfer sticker and the sticker was attached onto the surface of the specimen.
Measurement System
Recording an impact compression test from two directions using two HPV-X2 high-speed video cameras enables three-dimensional displacement measurement. Since a cylindrical specimen was used in this study, a three-dimensional displacement measurement was required. Accordingly, the test was recorded synchronously from two directions. Figs. 2 and 3 show the observation and test setup. The equipment used for recording the test is shown in Table 1. The video recorded by the HPV-X2 cameras were analyzed using the VIC-3D DIC software to determine strain distribution. Since VIC-3D can control HPV-X2 cameras, calibration and analysis can be performed easily.
Measurement Results
The test was recorded at 500,000 frames per second. Fig. 4 shows the results of 3D-DIC analysis. The analysis results indicate strain in the test direction. Since the specimen was compressed while constrained by the input bar and the output bar, strain in the tensile direction, though slight, is observed at both ends of the specimen. The results also show that as the test progressed, strain in the compression direction concentrated at the top of the specimen. This indicates that this test turned out not to be a genuine compression test and deformation was concentrated on one side.
Conclusion
Two HPV-X2 high-speed cameras were used for 3D-DIC analysis of a compression test by the Hopkinson bar method. In order to conduct a 3D-DIC analysis of an impact test, high-speed cameras that have a high recording speed and high resolution while also capable of synchronized recording from two directions are necessary. Equipped with all these features, the HPV-X2 is the optimal high-speed video camera for 3D-DIC analyses of impact tests.
Reference
1) Kichinosuke Tanaka and Yoji Adachi, Aeronautical and Space Sciences Japan, Volume 21, Issue 230 (1973)
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