• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2002년도 추계학술대회논문집
• /
• pp.652-657
• /
• 2002

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 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.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2002년도 추계학술대회논문초록집
• /
• pp.366.1-366
• /
• 2002

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 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 strong1y affected by them along with the flow coefficient. (omitted)

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
• /
• pp.137-142
• /
• 2000

The turbulent broadband sound power from a forward curved bladed fan can be modeled by the trailing edge noise. The trailing edge noise is usually influenced by inflow turbulence, separation, and boundary layer on the blade. This paper reports the effects of the solidity (C/s) and the stagger angles upon the trailing edge noise with respect to the trailing edge shapes of circular-arc cambered blade of multi-bladed fan, and discusses the major physical mechanism of reduced noise lot the circular trailing-edged case.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
• /
• pp.116-122
• /
• 2002

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 turbulenca 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.

• 한국유체기계학회 논문집
• /
• 제6권3호
• /
• pp.7-14
• /
• 2003

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.

• The Journal of the Acoustical Society of Korea
• /
• 제11권1E호
• /
• pp.50-55
• /
• 1992

팬의 익면 통과 주파수 소음은 총괄 소음 스펙트럼중에서 가장 명백한 성분이다. 그 소리는 일 반적으로 가장 불쾌한 성분이므로 저감이 요구된다. 따라서 그 소음치를 저감시키기 위해서는 정확한 축류형 팬의 소음원과 소음 방사 특성 규명이 요구된다. 본 연구에서는 푹류형 팬의 소음원과 소음 방 사 특성을 정의하였다. 음압 및 음향인텐시티를 이용한 음원 해석에서, 광센서를 이용한 축류형 팬의 동 기화가 수행되었고, 팬 날개에서의정확한 소음원의 위치를 결정하기 위해 Recording time의 결정이 제 안되었다. 팬 회전시, 소음원의 위치는 각 날개의 후단과 그 다음 날개의 선단사이에 각각 존재한다. 지 향성을 통하여 축류형 팬의 소음 방사 형태를 결정하였고, 벡터 에너지 흐름도로 음의 흐름을 가시화하 였다. 팬 익면에서의 회전 진동특성을 스트레인 게이지에 의하여 규명하였고, 또한 구조진동음의 음으로 의 기여도를 측정하였다. 또한 압전필름에 의한 팬 익면에서의 정압측정 가능성이 제시되었다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2000년도 춘계학술대회논문집
• /
• pp.396-401
• /
• 2000

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 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 solidity and the stagger angle upon the trailing edge noise from the circular arc-shaped blade of sirocco fan.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제29회 추계학술대회논문집
• /
• pp.305-310
• /
• 2007

엇회전식 축류팬의 복잡한 유동특성을 이해하고 설계, 공력 해석 및 소음 특성 예측에 활용될 수 있는 3차원 비정상 유동장을 측정하였다. 엇회전식 축류팬의 3차원 비정상 유동장은 작동 영역인 설계점에서 $45^{\circ}$ 경사 열선을 이용하여 전단 동익의 전방, 전단 동익과 후단 동익 사이 그리고 후단 동익의 후방의 수직 유로 단면에서 측정되었다. 엇회전식 축류팬의 전단 동익과 후단 동익에 의해 발생되는 후류, 팁 와류 및 팁 누설 유동의 비정상 특성을 속도 벡터와 속도 윤곽을 통해 나타내었다.

• 한국자동차공학회논문집
• /
• 제19권3호
• /
• pp.90-98
• /
• 2011

Noises from diesel engine are the major issues for noise pollution as well as affect customers' purchasing needs to vehicles powered by diesel engine. This study investigates to screen-out main factors that contribute to noises from diesel engine using VGT 2000cc engine developed recently. Changes of fuel temperature, intake temperature and the presence of three way catalyst don't affect the 'Engine Radiation Noise' and the solely three way catalyst influence on the 'Tail Pipe Noise'. Especially, there are no effects of the presence of three way catalyst on torque, which is main subject that should be considered in secondary study.