가변 입구 안내익이 있는 축류압축기의 성능예측 방법에 관한 연구

다국어 초록 (Multilingual Abstract)

In this study, numerical method, stage stacking method based on the result of numerical method and scaled stage stacking method have been applied to predict the performance of a multi-stage axial compressor with inlet guide vane. The results obtained through three different methods for off-design conditions were compared with performance test data. And the effect the angle of variable inlet guide vane was also investigated. The three-dimensional numerical simulation has been performed by using flow analysis program, FLUENT™ 6.3 and the performance prediction based on the stage stacking method has been performed with compressor analysis code from NASA.

참고문헌 (Reference)

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