- 진동하는 사각날개의 날개끌 와류 구조에 관한 실험적 연구
- ㆍ 저자명
- 현범수,김무롱,Hyun. Beom-Soo,Kim. Moo-Rong
- ㆍ 간행물명
- 大韓造船學會 論文集
- ㆍ 권/호정보
- 2006년|43권 1호|pp.59-67 (9 pages)
- ㆍ 발행정보
- 대한조선학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
Evolution of the unsteady three-dimensional tip vortex in the wake field of a rectangular NACA 0012 hydrofoil in pitching motion is investigated. Measurements were made in CWC using PIV. A hydrofoil has an aspect ratio of 5 with chord length of 1 Oem. Pitching angle and mean angle of attack were set to $pm$ $5^{circ}$ and $10^{circ}$, respectively. Frequency of oscillation was varied from 0.1 Hz to 1 Hz in order to study the effect of unsteadiness imposed by various frequencies, which correspond to the reduced frequency of K=0.1, 0.21, 0.52 and 1.05. Reynolds number based on chord length and free-stream velocity was $30 imes$$10^{4}$ Phase-averaging technique was employed. Unsteadiness and variation of the size and characteristics of tip vortex at different reduced frequency were discussed.