• Title/Summary/Keyword: 직선형 케스케이드

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A Study of Wall Shape Design for Cascade Experiment (케스케이드 실험을 위한 벽면형상 설계에 관한 연구)

  • Cho, Chong-Hyun;Cho, Bong-Soo;Kim, Chae-Sil;Cho, Soo-Yong
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03b
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    • pp.148-151
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    • 2008
  • In a double-passage cascade apparatus, only two blades are installed in order to increase the accuracy of experimental result by applying bigger blade than the size of multi-blades on the same apparatus. However, this causes difficulties to make correct periodic condition. In this study, sidewalls are designed to meet periodic condition without removing the operating fluid or adjusting tail boards. Surface Mach number on the blade surface is applied to a responsible variable, and 12 design variables which are related with sidewall profile control are selected. A gradient based optimization is adopted for wall design and CFX-11 is used for the internal flow computation. The computed result shows that it could obtain the same flow structure by modifying only the sidewalls of the double-passage cascade apparatus.

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An Experimental Study of the Performance on a Rotating Turbine with Various incidences (터빈입사각에 따른 회전하는 터빈의 성능에 관한 실험적 연구)

  • Cho, Chong-Hyun;Cho, Soo-Yong;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.9
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    • pp.94-102
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    • 2004
  • An experimental study on a rotating turbine is conducted with various incidence angles in order to find an optimum incidence angle. The incidence angle is an important design parameter in turbine blade design. however, most of experiments were conducted in a linear or annual cascade row. The suggested incidence angles from the experiments conducted in cascade rows could be unsuitable as a design parameter in the design of rotating parts. In this study, various incidence angles are applied and the turbine performance is measured in a rotating state. Experimental results show that the incidence on the rotor has a great influence on the turbine efficiency. The range of applicable incidence becomes narrow when the turbine operates at high input power. In the case of the tested rotor, the optimum incidence is about $-12^{\circ}$.