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An Alternative Simulation Method for Calculation of Microgas Flows under Flying Head Sliders

机译:计算飞行头滑块下微气体流量的另一种模拟方法

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The precise knowledge of the force and moment generated by the air squeezed under the read-write slider by the rotating disc is an engineering necessity in designing the air bearing surface slider. This paper reviews methods addressing the thin gas film bearings problem. It firstly reviews briefly the relatively well-known two methods of calculations of the microgas flows under flying head sliders, the generalized Reynolds equation, having given a number of useful results of slider design, and the DSMC method, which is precise and appropriate for the flow of complex configurations but is restricted to miniature (~micrometer) size sliders. The main purpose of the paper is to introduce to the reader an alternative method, the information preservation (IP) method, for use in simulation of the flows under air bearing surfaces. Some recent results of IP simulation of slider flows published on conference proceedings are introduced here.
机译:在设计空气轴承表面滑块时,要准确地了解由旋转磁盘在读写滑块下方挤压的空气所产生的力和力矩,这是工程设计的必要条件。本文回顾了解决薄气膜轴承问题的方法。首先,它简要回顾了相对较著名的两种计算飞行头滑块下的微气体流量的方法:广义雷诺方程(给出了滑块设计的许多有用结果)和DSMC方法,该方法精确且适用于复杂配置的流程,但仅限于微型(〜微米)大小的滑块。本文的主要目的是向读者介绍一种可供选择的方法,即信息保存(IP)方法,用于模拟空气轴承表面下的流动。在此介绍在会议记录中发布的滑块流程的IP仿真的一些最新结果。

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