Cite
Fatigue Crack Growth of SLM Ti-4Al-6V Processed by Ultrasonic Impact Treatment.
MLA
Eremin, A. V., et al. “Fatigue Crack Growth of SLM Ti-4Al-6V Processed by Ultrasonic Impact Treatment.” AIP Conference Proceedings, vol. 2167, no. 1, Nov. 2019, pp. 20082-1-20082–84. EBSCOhost, https://doi.org/10.1063/1.5131949.
APA
Eremin, A. V., Burkov, M. V., Panin, S. V., & Byakov, A. V. (2019). Fatigue Crack Growth of SLM Ti-4Al-6V Processed by Ultrasonic Impact Treatment. AIP Conference Proceedings, 2167(1), 20082-1-20082–20084. https://doi.org/10.1063/1.5131949
Chicago
Eremin, A. V., M. V. Burkov, S. V. Panin, and A. V. Byakov. 2019. “Fatigue Crack Growth of SLM Ti-4Al-6V Processed by Ultrasonic Impact Treatment.” AIP Conference Proceedings 2167 (1): 20082-1-20082–84. doi:10.1063/1.5131949.