The method of definition of pressure on input and an output of thin lubricant spheres of a flat aerostatic support of linear engines which are described by non-stationary equation Reynoldsa is developed and experimental researches by definition of dependence of pressure from a backlash are carried out, dependences of specific elevating force of a flat aerostatic support on pressure in points submissions of air are determined. When you are citing the document, use the following link http://essuir.sumdu.edu.ua/handle/123456789/1082
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