2015
DOI: 10.1016/j.triboint.2014.12.002
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A flow-difference feedback iteration method and its application to high-speed aerostatic journal bearings

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Cited by 27 publications
(14 citation statements)
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“…The finite difference method is one of the commonly used methods for solving Reynolds equation. Yazhe Li proposes a novel iteration method for finite difference method‐based solution of Reynolds equation and applies it to the analysis of high‐speed aerostatic journal bearings . This paper uses the finite difference method to solve perturbation pressure Equation , and the program flow chart of solving equation is as follows (Figure ).…”
Section: Dynamics Model Of Hydrostatic Bearing Rotor Systemmentioning
confidence: 99%
“…The finite difference method is one of the commonly used methods for solving Reynolds equation. Yazhe Li proposes a novel iteration method for finite difference method‐based solution of Reynolds equation and applies it to the analysis of high‐speed aerostatic journal bearings . This paper uses the finite difference method to solve perturbation pressure Equation , and the program flow chart of solving equation is as follows (Figure ).…”
Section: Dynamics Model Of Hydrostatic Bearing Rotor Systemmentioning
confidence: 99%
“…Yapılan bu çalışma ile elde edilen sonuçlar [10], [22] ve [31] çalışmalarda yer alan üç boyutlu basınç dağılımı grafikleri ile karşılaştırıldığında, her ne kadar basınçlı hava yataklarının geometrik özellikleri ve çalışma parametreleri farklı da olsa, birleşme çizgisi üzerindeki basınç değerlerinin, orifislerdeki maksimum basıncın ve orifislerden yatak kenarlarına dağılan basıncın formsal olarak uygunluk gösterdiği görülmüştür. Bu çalışma ile elde edilen diğer bir sonuç ise; Reynold's denkleminin nümerik çözümünde kullanılan dikdörtgen gridin birleşme çizgisi üzerindeki noktaların basınç değerlerinin yüksek mertebeden geri ve ileri farklar kullanılarak elde edilebileceğidir.…”
Section: Sonuçlar (Conclusion)unclassified
“…Increasing the supply pressure is the second approach. 13,17,22 However, the stability of aerostatic bearings decreases and the self-excited micro-vibration or the pneumatic hammer probably occur when the supply pressure increases. 23,24 The third approach is to use recess structure such as pockets or grooves on the aerostatic bearing surface.…”
Section: Introductionmentioning
confidence: 99%