• Title/Summary/Keyword: 익렬간 혼합 모델

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Numerical calculation of torque converter flow using interrow mixing model (익렬간 혼합모델을 이용한 토크 컨버터 유동장의 수치계산)

  • Park, Jae-In;Jo, Gang-Rae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.22 no.3
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    • pp.326-335
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    • 1998
  • In this study, a steady three-dimensional incompressible turbulent flow within a torque converter was numerically analyzed with the introduction of interrow mixing model. Mixing planes were introduced to exchange the flow informations between two adjacent elements of the torque converter. The mixing planes were installed among three elements of the torque converter. Therefore, in the present method, it could be possible to calculate the flow-filed within the torque converter without any assumption of circulating flow rates or any extension of boundaries toward the upstream and the downstream for each element. The numerically calculated performances of the torque converter were in good agreement with experimental results, and the complex flow patterns were be observed according to design and off-design condition. As a conclusion, it was found that the present numerical method was very effective in the steady flow analysis of torque converters.

Performance Prediction of the 1-Stags Axial Fan using Steady Coupled Blade Row Calculation Model (정상 간섭 익렬 계산 모델을 용한 1단 축류 송풍기의 성능 예측)

  • Sohn, Sang-Bum;Joo, Won-Gu;Cho, Kang-Rae
    • 유체기계공업학회:학술대회논문집
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    • 1998.12a
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    • pp.49-54
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    • 1998
  • The flow inside an axial turbomachinery with multi-stage can be characterized as unsteady phenomena. In order to predict accurately these complex unsteady flow patterns including rotor-stator interaction effects, enormous computer resources are required. So it is not compatible in preliminary design process. In this study, steady coupled blade row flow with rotor-stator interaction solver is developed using interrow mixing model and used to predict the performance of the axial fan. To verify the computational method, the calculations are compared with experimental results and show satisfactory agreement with them. The interaction effects on the performance of the axial fan have also been studied by comparing the results of steady coupled blade row and steady single blade row flow calculation.

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