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KC-100 항공기 주날개의 결빙에 의한 공력 영향성 연구
이창훈(C.H. Lee),신성민(S.M. Sin),정성기(S.K. Jung),명노신(R.S. Myong),조태환(T.H. Cho),정재홍(J.H. Jung),정훈화(H.H. Jeong) 한국전산유체공학회 2010 한국전산유체공학회 학술대회논문집 Vol.2010 No.5
Ice accretion on aircraft surface in icing condition induces external shape changes that may result in a hazard factor for aircraft safety. In case of aircraft main wing with high lift equipment, ice accretion is observed around leading edge and flap. During the design phase, location of ice accretion and associated aerodynamic characteristics must be investigated. In this study, icing effects on aerodynamic characteristics of the main wing section of KC-100 aircraft are investigated using an Eulerian-based FENSAP-ICE code in various icing conditions.