한국전산유체공학회:학술대회논문집
- 2010.05a
- /
- Pages.460-463
- /
- 2010
EULERIAN-BASED ANALYSIS SYSTEM FOR SIMULATION OF AIRFOIL ICING
Eulerian 기반 에어포일 결빙 해석 시스템 연구
- Jung, S.K. ;
- Oh, J.G. ;
- Chun, S.H. ;
- Moon, H. ;
-
Myong, R.S.
;
- Cho, T.H.
- 정성기 (경상대학교 기계항공공학부 대학원) ;
- 오진근 (경상대학교 기계항공공학부 대학원) ;
- 전수환 (경상대학교 기계항공공학부 대학원) ;
- 문혁 (경상대학교 기계항공공학부 대학원) ;
-
명노신
(경상대학교 기계항공공학부 및 항공기부품기술연구소)
;
- 조태환 (경상대학교 기계항공공학부 및 항공기부품기술연구소)
- Published : 2010.05.13
Abstract
Ice accretion on aircraft surface can greatly impair the aerodynamic performance of aircraft. As an alternative to the traditional Lagrangian particle tracking approach, an Eulerian-based droplet impingement and ice accretion code for air flows containing water droplets was developed A CFD solver was also developed to solve the clean airflow. The results of present method were compared with experimental data and previous icing codes such as LEWICE and FENSAP-ICE and were confirmed to show good agreement each other in qualitative and quantitative ways.
Keywords