The direct simulation Monte Carlo method (DSMC) is used to study rarefied gas flow between an inclined plane slider bearing and a nano channel representing one groove in a discrete track recording head/disk interface. The forces acting on the slider are investigated as a function of slider pitch angle, disk velocity, track pitch, groove width, and groove depth. The influence of the absolute groove size on the slider forces is found to be small.
机构:
NASA, Langley Res Ctr, Div Space Syst, Aerothermodynam Branch, Hampton, VA 23665 USANASA, Langley Res Ctr, Div Space Syst, Aerothermodynam Branch, Hampton, VA 23665 USA