성능 및 소음 해석 기능이 수반된 전산화된 축류 송풍기 설계 체제

다국어 초록 (Multilingual Abstract)

A computerized axial flow fan design system is developed with the capabilities for predicting the aerodynamic performance and the noise characteristics of fan. In the present study, the basic fan blading design is made by combining vortex distribution scheme with camber line design, airfoil selection, blade thickness distribution and stacking of blade elements. With the designed fan blade geometry, the through-flow field and the performance of fan are analyzed by using the streamline curvature computing scheme with spanwise total pressure loss and flow deviation models. Fan noise is assumed to be generated due to the pressure fluctuation induced by wake vortices of fan blades and to radiate as dipole distribution. The vortex-induced fluctuating pressure on blade surface is calculated by combining thin airfoil theory and the predicted flow field data. The predicted performances, sound pressure level and noise directivity patterns of fan by the present method are favorably compared with the test data of actual fans. Furthermore, the present method is shown to be very useful in designing the blade geometry of new fan and optimizing design variables of the fan to achieve higher efficiency and lower noise level.

목차 (Table of Contents)

• ABSTRACT
  
• 1. 서론
  
• 2. 전산 프로그램의 이론적 배경 및 구성
  
• 3. 적용 사례
  
• 4. 결과의 검증
  
• 5. 결론
  
• 참고문헌