2009
DOI: 10.1007/s00542-009-0859-5
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Plane strain sliding contact of multilayer magnetic storage thin-films using the finite element method

Abstract: The sliding contact or scratch behavior of multi-layer thin-films such as those found in magnetic storage disks has been studied using the finite element method. A rigid cylinder sliding over a multilayered thinfilm half-space was implemented to simulate the contact between a feature of the recording slider (such as the protrusion on the trailing edge of the slider, which is part of the thermal flying-height control, TFC) and the magnetic storage multilayer disk. The effects of different parameters such as nor… Show more

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Cited by 17 publications
(7 citation statements)
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“…While the steady-state value of the shear traction might be within the limits required to avoid plastic deformation in the DLC layer, the large variation due to vibrations after TD, as shown in figure 16(b), could cause damage to the disk. Specifically, the hardness of DLC is taken to be approximately equal to 1.8 times its yield strength [27], so its yield strength which is calculated to be 7.2 GPa, is larger than the maximum shear traction of 6.69 GPa at 12.2 nm of actuation as shown in figure 16(a).…”
Section: Assessment Of Contact Severitymentioning
confidence: 99%
“…While the steady-state value of the shear traction might be within the limits required to avoid plastic deformation in the DLC layer, the large variation due to vibrations after TD, as shown in figure 16(b), could cause damage to the disk. Specifically, the hardness of DLC is taken to be approximately equal to 1.8 times its yield strength [27], so its yield strength which is calculated to be 7.2 GPa, is larger than the maximum shear traction of 6.69 GPa at 12.2 nm of actuation as shown in figure 16(a).…”
Section: Assessment Of Contact Severitymentioning
confidence: 99%
“…The steady state average value of the shear traction at a TFC actuation of 13 nm is 6.64 GPa. This is smaller than the yield strength of DLC, which can be calculated from its hardness to be 7.2 GPa (Katta et al 2009). The average steady state mean pressure for the same actuation is 4.88 GPa and is smaller than the DLC hardness of 13 GPa.…”
Section: Flyability Results For the Optimized Designmentioning
confidence: 99%
“…The study of the configuration that optimises the performance of the layered system to better accommodate contact load is a subject of interest [1,2] considering the cracking and damage modes that affect the contact fatigue life. With analytical solutions lacking even for homogeneous materials under contact load, various specialised numerical methods were developed in computational contact mechanics, seeking numerical solutions for the contact area, deformation and stresses arising in the contacting bodies: (a) the finite element method [3][4][5][6][7][8], (b) the boundary element method [9], (c) the equivalent inclusion method [10][11][12], and (d) the semi-analytical method (SAM) [13][14][15][16][17][18][19][20][21][22]. The latter is particularly efficient when coupled with Fourier transform algorithms that provide means for rapid calculation of convolution products, by converting the tedious integration operation from the problem space domain, into element-wise multiplication in an associated frequency domain.…”
Section: Introductionmentioning
confidence: 99%