- 항공기 주위 난류 유동장 해석
- ㆍ 저자명
- 김윤식,박수형,권장혁,Kim. YoonSik,Park. Soo Hyung,Kwon. Jang-Hyuk
- ㆍ 간행물명
- 한국전산유체공학회지
- ㆍ 권/호정보
- 2005년|10권 4호|pp.39-50 (12 pages)
- ㆍ 발행정보
- 한국전산유체공학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
An application of the KFLOW3D code which has been developed at KAIST is presented. This paper briefly describes the underlying methodology and summarizes the results for the DLR-F6 transport configuration recently presented in the second AIAA CFD Drag Prediction Workshop held in Orlando, FL, June 2003. KFLOW3D is a parallelized Reynolds averaged Navier-Stokes solver for multi-block structured grids. For the present computations, 2-equation k-$omega$ WD+ nonlinear eddy viscosity model is used. The emphasis of the paper is placed on the implementation of the k-$omega$ WD+ model in the multigrid framework and practicality of KFLOW3D for accurately predicting not only the integrated aerodynamic property such as the drag coefficient but pressure distributions.