- 3차원 축류형 터빈익형의 공력설계에 관한 연구
- ㆍ 저자명
- 장범익,김동식,조수용,Jang. B.I.,Kim. D.S.,Cho. S.Y.
- ㆍ 간행물명
- 한국동력기계공학회지
- ㆍ 권/호정보
- 2001년|5권 3호|pp.38-47 (10 pages)
- ㆍ 발행정보
- 한국동력기계공학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
One stage axial type turbine is designed by mean-line analysis, streamline curvature method and blade design method using shape parameters. Tip and hub diameter of the turbine are 300mm and 206.4mm, respectively. The rotating speed is 1800RPM, and the output power is 1.4kW. The flow coefficient is 1.68 and the reaction factor at mean-line is 0.373. The number of stator and rotor of the turbine are 31 and 41, respectively. Mach number of stator exit flow near hub is 0.164. A test rig is developed for performance test to validate a developed design method. The experimental result shows that the maximum efficiency is obtained on the design point.