- 익렬 날개 후단소음의 저감
- ㆍ 저자명
- 손정민,김휘중,이승배,조성민,Son. J.M.,Kim. H.J.,Lee. S.B.,Cho. S.M.
- ㆍ 간행물명
- 유체기계저널
- ㆍ 권/호정보
- 2003년|6권 3호|pp.7-14 (8 pages)
- ㆍ 발행정보
- 유체기계공업학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
It is addressed that the turbulent broadband sound power from a sirocco fan can be modeled by the trailing edge noise. The trailing edge noise is usually influenced by inflow turbulence, separation, and boundary layer thickness on the blade. The design parameters such as solidity (c/s) and stagger angle are specified to predict performance and noise level because the separation and slip velocity are strongly affected by them along with the flow coefficient. This paper reports the effects of the stagger angle upon the trailing edge noise for various trailing edge shapes. It is believed that the serrated trailing edge provides break-up mechanism for organized convecting vortices, thereby reduce the overall noise level for every case of stagger angle.