Effect of Pressure Difference across Bearing on Characteristics of Cryogenic Hydrostatic Journal Bearing
The effect of the pressure difference across a bearing on the characteristics of the cryogenic hydrostatic journal bearing used in the liquid fuel turbopump of rocket engines in space transport systems is numerically analyzed. The bearing has many recesses arranged in two rows in a staggered manner....
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Veröffentlicht in: | TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series C 1997/03/25, Vol.63(607), pp.995-1001 |
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Sprache: | eng ; jpn |
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