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International Journal of Rotating Machinery
Volume 2008, Article ID 426023, 7 pages
Research Article

The Application of Counter-Rotating Turbine in Rocket Turbopump

1Institute of Engineering Thermophysics, Chinese Academy of Sciences, P.O. Box 2706, Beijing 100080, China
2Graduate School of Chinese Academy of Sciences, P.O. BOX 2706, Beijing 100080, China

Received 1 May 2007; Revised 20 August 2007; Accepted 31 October 2007

Academic Editor: Chunill Hah

Copyright © 2008 Tang Fei et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. Z. Yuanju, Design of Liquid Rocket Turbopump, BUAA Press, Beijing, China, 1995.
  2. T. Wintucky and W. L. Stewart, “Analysis of two stage counter rotating turbine: efficiencies in terms of work and speed requirements,” 1958, NACA RM E57L0. View at Google Scholar
  3. Y. Naruo, N. Tanatsugu, and K. Kuratani, “Development study of LOX/LH2 propulsion system in ISAS,” 1984, IST. View at Google Scholar
  4. F. W. Huber and J. P. Veres, “Design and test of a small two counter rotating turbine for rocket engine application,” 1993, AIAA Paper 93-213. View at Google Scholar
  5. D. P. Davidson and A. K. Finke, “The design and fabrication of a small highly instrumented counter rotating turbine rig,” 1993, ASME 93-GT-39. View at Google Scholar
  6. J. P. Veres, “Two stage turbine for rockets,” 1994, NASA N94 2466. View at Google Scholar
  7. L. W. Griffin and F. W. Huber, “Turbine technology team: an overview of current and planned activities relevant to the national launch system,” 1992, AIAA 92-322. View at Google Scholar
  8. F. W. Huber and L. W. Griffin, “Design of advanced turbopump drive turbines for national launch system application,” 1992, AIAA 92-322. View at Google Scholar
  9. A. Yamamoto, “Recent fundamental research on turbine steady and unsteady aerodynamics at the national aerospace laboratory in Japan proceedings of colloquium on turbomachinery,” 1996. View at Google Scholar
  10. A. Yamamoto and E. Outa, “Low speed annular cascade tests of an ultra-highly loaded turbine with tip clearance, part I—near design incidence,” 1999, ASME 99-GT-21. View at Google Scholar
  11. T. Kawakami and A. Yamamoto, “Investigation of flow in pltra-highly loaded turbine cascade by PTV method,” in 8th International Symposium on Flow Visualization, January 1998.
  12. A. Yamamoto, T. Matsunuma, and E. Outa, “Three dimensional flows and losses in an ultra-highly loaded turbine,” 1998, ISROMAC-. View at Google Scholar
  13. C. Hah, Turbomachinery Fluid Dynamics and Heater Transfer, Marcel Dekker, New York, NY, USA, 1995.
  14. 1997, Twin Rotor Turbopump Program Progress Report, Contract NAS8-9716.
  15. P. Pempie and L. Ruet, “Counter rotating turbine designed for turbopump rocket engine,” 2003, AIAA Paper 2003-476. View at Google Scholar
  16. W. R. Briley and P. D. Johnson, “Computation of flow past a turbine blade with and without tip clearance,” Journal of Propulsion Technology, vol. 12, no. 6, 1991, ASME 91-GT-56, 1991Yan Zichu: Development of Liquid rocket turbopump technolog. View at Google Scholar
  17. J. Lucheng, Z. Wentao, and X. jianzhong, “Primary analysis and design of a vaneless counter rotating turbine,” Journal of Engineering Thermophysics, vol. 22, no. 2, 2001. View at Google Scholar
  18. W. L. Stewart, “Analytical investigation of multistage turbine efficiency characteristics in terms of work and speed requirements,” 1958, NACA RM E57k22. View at Google Scholar
  19. F. M. White, Fluid Mechanics, McGraw-Hill, New York, NY, USA, 4th edition, 2000.
  20. P. P. Walsh and P. Fletcher, Gas Turbine Performance, Blackwell Science, Oxford, UK, 2nd edition, 2004.