Numerical Analysis of Unshrouded Impeller Flowfield in the LE-X Liquid Hydrogen Pump

Author(s):  
Hideyo Negishi ◽  
Shinji Ohno ◽  
Yohei Ogawa ◽  
Kenji Aoki ◽  
Teiu Kobayashi ◽  
...  
Author(s):  
Nobuhiro Yamanishi ◽  
Miki Nishimoto ◽  
Syuusuke Hori ◽  
Koichi Okita ◽  
Chisachi Kato ◽  
...  

1970 ◽  
Author(s):  
J. CONNELL ◽  
J. HENSHALL ◽  
W. TUCKER

1964 ◽  
Author(s):  
W. N. Hall ◽  
P. Hildebrand ◽  
D. S. Ko

2003 ◽  
Vol 19 (3) ◽  
pp. 356-363 ◽  
Author(s):  
Masaharu Uchiumi ◽  
Kenjiro Kamijo ◽  
Kunio Hirata ◽  
Akira Konno ◽  
Tomoyuki Hashimoto ◽  
...  

2009 ◽  
Vol 22 (3) ◽  
pp. 303-315 ◽  
Author(s):  
D. Baraldi ◽  
A.G. Venetsanos ◽  
E. Papanikolaou ◽  
M. Heitsch ◽  
V. Dallas

1999 ◽  
Vol 121 (4) ◽  
pp. 879-885 ◽  
Author(s):  
Hiroyuki Yoshikawa ◽  
Terukazu Ota ◽  
Kazuyuki Higashino ◽  
Shunichiro Nakai

Dynamic 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.


1996 ◽  
Vol 32 (5) ◽  
pp. 5025-5027 ◽  
Author(s):  
Y. Abe ◽  
A. Nakagawa ◽  
M. Watada ◽  
S. Torii ◽  
K. Yamane ◽  
...  

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