한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2001년도 제17회 학술발표회 논문초록집
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- Pages.11-14
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- 2001
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- 1975-342X(pISSN)
부분흡입노즐방식의 터빈시스템에 대한 성능 평가
Performance Evaluations for the Partial-Admission Type Turbine System
초록
3-D compressible flow analysis was conducted by using mixing plane method for turbine system which is consisted of partial admission nozzle and rotor. Computational results are shown oblique shock wave in blade leading and trailing edge and also shown flow separation along suction surface of blade due to abrupt blade curvature. But computational results are well agree with 1-D calculation results and experimental data.
키워드