3차원 가스터빈 블레이드의 연성 해석에 관한 연구
A turbine blade operates under high temperature, high pressure, and the loads have the characteristics that the amplitudes change. Therefore, it is important to perform a stress analysis considering thermal and pressure loads. The purpose of this study is to investigate the effects of these loads on...
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| Veröffentlicht in: | 한국생산제조학회지 2006, 15(2), , pp.38-43 |
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| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | kor |
| Schlagworte: | |
| Online-Zugang: | Volltext |
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| Zusammenfassung: | A turbine blade operates under high temperature, high pressure, and the loads have the characteristics that the amplitudes change. Therefore, it is important to perform a stress analysis considering thermal and pressure loads. The purpose of this study is to investigate the effects of these loads on gas turbine blade through thermal stress analysis. The analysis results shows that pressure in gas fluid flow around blade is high in leading edge part, Gas temperature is connections with pressure of flow around blade. The distribution of stress from blade is appearing as is different at suction side and pressure side. KCI Citation Count: 1 |
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| ISSN: | 2508-5093 2508-5107 |