축류형 흡입송풍기 설계기술에 관한 연구A Study of Design Method of an Axial-Type Suction Fan
- Other Titles
- A Study of Design Method of an Axial-Type Suction Fan
- Authors
- 최형준; 김창수; 조종현; 조수용
- Issue Date
- 2010
- Publisher
- 한국유체기계학회
- Keywords
- Axial-Type Fan(축류형송풍기); Blade Design(익형설계); Suction Fan(흡입송풍기); Aerodynamic Design(공력설계); Performance Prediction(성능예측)
- Citation
- 한국유체기계학회 논문집, v.13, no.1, pp 44 - 54
- Pages
- 11
- Indexed
- KCI
- Journal Title
- 한국유체기계학회 논문집
- Volume
- 13
- Number
- 1
- Start Page
- 44
- End Page
- 54
- URI
- https://scholarworks.gnu.ac.kr/handle/sw.gnu/25884
- ISSN
- 2287-9706
- Abstract
- Many different types of fan have been applying to various industrial fields. Fan design methods are much different depending on the types of fan, operating conditions, and connecting parts at the inlet or exit of the fan etc. In this study, design methods for an axial-type suction fan are studied. This fan discharges the air in the relative static pressure of -285Pa to the atmosphere with the flow rate of 960m3/min. For three-dimensional blade design, three different design methods were applied, such as the free vortex method, the exponential method, and the cascade method. In the cascade method, the blade loading along the radial direction was obtained from the lift coefficient which was necessary to obtain the pressure rise on a fan rotor. This method is different from the free vortex and the exponential method which control the strength of the vortex. The fan performance prediction was conducted using the CFD with three different inlet ducts. The best fan performance was obtained when the fan was designed by using the cascade method. The designed fan using the exponential method showed better performance compared to a fan designed using the free vortex method. However, the fan performance was changed depending on the installed inlet ducts. So, an efficient fan can be designed with the adjustment of design variables on the basis of the flow structures within the fan as well as the fan design procedure.
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Collections - 공과대학 > Department of Aerospace and Software Engineering > Journal Articles

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