journal article·2015-07-01Open access

Analytical modelling for ultrasonic surface mechanical attrition treatment

Guan-Rong Huang, W. Y. Tsai, J. C. Huang, Chin-Kun Hu

AIP Advances· Volume 5· Issue 7

Abstract

The grain refinement, gradient structure, fatigue limit, hardness, and tensile strength of metallic materials can be effectively enhanced by ultrasonic surface mechanical attrition treatment (SMAT), however, never before has SMAT been treated with rigorous analytical modelling such as the connection among the input energy and power and resultant temperature of metallic materials subjected to SMAT. Therefore, a systematic SMAT model is actually needed. In this article, we have calculated the averaged speed, duration time of a cycle, kinetic energy and kinetic energy loss of flying balls in SMAT for structural metallic materials. The connection among the quantities such as the frequency and amplitude of attrition ultrasonic vibration motor, the diameter, mass and density of balls, the sample mass, and the height of chamber have been considered and modelled in details. And we have introduced the one-dimensional heat equation with heat source within uniform-distributed depth in estimating the temperature distribution and heat energy of sample. In this approach, there exists a condition for the frequency of flying balls reaching a steady speed. With these known quantities, we can estimate the strain rate, hardness, and grain size of sample.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Surface Treatment and Residual Stress · Erosion and Abrasive Machining · High-Velocity Impact and Material Behavior

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

National Taiwan University 1 Department of Physics, , Taipei, Taiwan 106, ROC

National Sun Yat-Sen University 2 Department of Materials and Optoelectronic Science, , Kaohsiung, Taiwan 804, ROC

Institute of Physics 3 , Academia Sinica, Nankang, Taipei, Taiwan 115, ROC

References (19)

Show source-provided references
1. Finite Elements in Analysis and Design · 1999 · 30 · 17910.1016/S0168-874X(98)00057-2 ↗
2. International Journal of Fatigue · 1998 · 20 · 35110.1016/S0142-1123(98)00002-4 ↗
3. Nanostruct. Mater. · 1999 · 11 · 43310.1016/S0965-9773(99)00324-4 ↗
4. Mater Sci Eng A. · 2000 · 286 · 9110.1016/S0921-5093(00)00686-9 ↗
5. Acta Mater. · 2010 · 58 · 508610.1016/j.actamat.2010.05.044 ↗
6. Acta Mater. · 2002 · 50 · 460310.1016/S1359-6454(02)00310-5 ↗
7. Acta Mater. · 2003 · 51 · 187110.1016/S1359-6454(02)00594-3 ↗
8. Acta Mater. · 2006 · 54 · 528110.1016/j.actamat.2006.07.013 ↗
9. Mater. Sci. Eng. A. · 2004 · 375 · 3810.1016/j.msea.2003.10.261 ↗
10. Acta Mater. · 2005 · 53 · 68110.1016/j.actamat.2004.10.021 ↗
11. Acta Mater. · 2004 · 52 · 410110.1016/j.actamat.2004.05.023 ↗
12. Acta Mater. · 2002 · 50 · 207510.1016/S1359-6454(02)00051-4 ↗
13. Materials Science Forum. · 2008 · 579 · 9110.4028/www.scientific.net/MSF.579.91 ↗
14. Physical review B · 1998 · 58 · 1108510.1103/PhysRevB.58.11085 ↗
15. Physical review B · 2001 · 64 · 22410510.1103/PhysRevB.64.224105 ↗
16. Physical review B · 2002 · 66 · 08540410.1103/PhysRevB.66.085404 ↗
17. Scripta Mater. · 2015 · 103 · 4510.1016/j.scriptamat.2015.03.003 ↗
18. Adv. Eng. Mater. · 2003 · 5 · 36510.1002/adem.200310079 ↗
19. 1989