한국유체기계학회 논문집 (The KSFM Journal of Fluid Machinery)

한국유체기계학회 (Korean Society for Fluid machinery)
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Numerical Flow Analysis of a Partial Admission Turbine Using a Frozen Rotor Method

  • 노준구 (한국항공우주연구원 터보펌프개발그룹) ;
  • 정은환 (한국항공우주연구원 터보펌프개발그룹) ;
  • 이은석 (한국항공우주연구원 터보펌프개발그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프개발그룹)
  • 발행 : 2004.12.01
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초록

Numerical analysis of the partial admission turbine in the KARI turbopump has been performed. Flow field of the partial admission turbine is intrinsically unsteady and three dimensional. To avoid heavy computational efforts, the frozen rotor method is adopted in computation and compared with the mixing plane approach. The frozen rotor method can represent the variation of a flow field along the circumferential direction of rotor blades, which have the different relative positions to the nozzle with one another. It also illustrates the wake loss mechanism starting from the lip of a nozzle, which is not captured in the mixing plane method. The frozen rotor method has proven to be an efficient tool for the design of a partial admission turbine.

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참고문헌

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  6. Lee, E. S. and Kim, J., 2003, 'Numerical Studies of Geometrical Design Variables for Improvement of Aerodynamic Performance of Supersonic Impulse Turbine,' Proceedings of The 12th International Conference on Fluid Flow Technology, September, Budapest, pp. 1246-1250
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피인용 문헌

  1. A Numerical Study on the Performance Characteristics of a Partial Admission Axial Supersonic Turbine with Swept Rotor Blades vol.17, pp.3, 2013, https://doi.org/10.6108/KSPE.2013.17.3.001