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초록
The rotor blade of ducted fan for multi ducted fan UAV is designed. The multi ducted fan UAV can reconnoiter, observe in the town and small area. The ducted fan has a good efficiency and long duration of flight. The rotor blade of ducted fan is designed by simplified meridional flow analysis method. This method supposed complicated flow to be two-dimensional axisymmetric, blade element flow. The stacking line of designed rotor for ducted fan is changed, then the design results are verified by frequency panel method.
키워드
stacking line(스태킹 라인); Ducted fan(덕티드 팬); Frequency Domain Panel method(주파수영역 패널법); Rotor(동익)
- 제목
- Stacking Line 변화를 고려한 멀티덕티드팬 무인항공기용 덕티드팬 로터의 공력 설계
- 제목 (타언어)
- Aerodynamic Design of Ducted Fan Rotor for Multi Ducted Fan UAV by Alteration of Stacking Line
- 저자
- 류민형; 조이상; 조진수
- 발행일
- 2012-04
- 유형
- Proceeding
- 저널명
- 한국항공우주학회 2012년도 춘계학술대회
- 페이지
- 39 ~ 43