02161nam 2200565I 450 991070529460332120140409145419.0(CKB)5470000002448416(OCoLC)876159712(EXLCZ)99547000000244841620140409j201307 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierA non-cut cell immersed boundary method for use in icing simulations /Christian M. Sarofeen and Ralph W. Noack, Richard E. KreegerCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,July 2013.1 online resource (31 pages) illustrations (some color)NASA/TM ;2013-217881Title from title screen (viewed on Apr. 9, 2014)."July 2013.""Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012.""AIAA-2012-1204."Includes bibliographical references (page 31).Aerodynamic coefficientsnasatAerodynamic dragnasatComputational fluid dynamicsnasatControl surfacesnasatFinite volume methodnasatIce formationnasatPressure distributionnasatAerodynamic coefficients.Aerodynamic drag.Computational fluid dynamics.Control surfaces.Finite volume method.Ice formation.Pressure distribution.Sarofeen Christian M.1415889Noack Ralph W.Kreeger Richard E.NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910705294603321A non-cut cell immersed boundary method for use in icing simulations3519292UNINA