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contributor authorHiroyuki Yoshikawa
contributor authorKazuyuki Higashino
contributor authorShunichiro Nakai
contributor authorTerukazu Ota
date accessioned2017-05-09T00:00:57Z
date available2017-05-09T00:00:57Z
date copyrightOctober, 1999
date issued1999
identifier issn0742-4787
identifier otherJOTRE9-28684#879_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122844
description abstractDynamic characteristics of a two row staggered recess cryogenic hydrostatic journal bearing used in the liquid hydrogen turbopump of rocket engines for space transport systems are numerically analyzed. Effects of the rotational speed and the shaft eccentricity are studied in the analysis. Their effects on the stiffness and damping coefficients and the whirl frequency ratio are clarified. Moreover, effects of the orifice parameter, the distance between two recess rows, and the number of recesses on these dynamic characteristics are investigated.
publisherThe American Society of Mechanical Engineers (ASME)
titleNumerical Analysis on Dynamic Characteristics of Cryogenic Hydrostatic Journal Bearing
typeJournal Paper
journal volume121
journal issue4
journal titleJournal of Tribology
identifier doi10.1115/1.2834150
journal fristpage879
journal lastpage885
identifier eissn1528-8897
keywordsNumerical analysis
keywordsHydrostatics
keywordsJournal bearings
keywordsDamping
keywordsHydrogen
keywordsRocket engines
keywordsStiffness AND Whirls
treeJournal of Tribology:;1999:;volume( 121 ):;issue: 004
contenttypeFulltext


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