Cavitation instabilities of an inducer in a cryogenic pump

Author:

Kim Dae-Jin,Sung Hyung Jin,Choi Chang-Ho,Kim Jin-Sun

Funder

Creative Research Initiatives

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. S.Rush, L.Hall, Tutorial on cryogenic submerged electric motor pumps, in: Proceedings of the 18th International Pump Users Symp., Houston, Texas, 2001.

2. Modern Engineering for Design of Liquid-Propellant Rocket Engines;Huzel,1992

3. Thermodynamic effect on a cavitating inducer—Part I: geometrical similarity of leading edge cavities and cavitation instabilities;Franc;J. Fluids Eng.,2010

4. W.G. Lester, A.S.M., D. Phil, Temperature and fluid property effects on cavitation in aircraft fuel pumps, in: Aeronautical Research Council, C.P. 1128, 1969.

5. Experimental study of rotating cavitation of rocket propellant pump inducers;Hashimoto;J. Propuls. Power,1997

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