- 콴다효과를 응용한 플랩이 달린 고양력 날개장치에 대한 실험적 연구
- ㆍ 저자명
- 안해성,김효철
- ㆍ 간행물명
- 大韓造船學會 論文集
- ㆍ 권/호정보
- 2003년|40권 5호|pp.10-16 (7 pages)
- ㆍ 발행정보
- 대한조선학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
To investigate the jet effect on circulation control, a segment of model was prepared and inserted horizontally across the test section of the cavitation tunnel. The hydrodynamic forces acting on the model were measured under the 2 dimensional flow behavior. Circulation flow control requires higher flow rate of water jet than boundary layer control does. Jet injection is effective in increasing lift coefficient and the increments reach to 160% in a certain combination of parameters such as an angle of attack, jet flow rate and flap angle. The blown water jet not only reduces form drag but also thrust effect, which is sometimes greater than the form drag in specific conditions.