01867nam 2200469I 450 991070794420332120170207133449.0(CKB)5470000002469127(OCoLC)971548660(EXLCZ)99547000000246912720170207j201609 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierIce-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel /Andy P. Broeren [and five others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,September 2016.1 online resource (34 pages) color illustrationsNASA/TM ;2016-219137"September 2016.""Prepared for the 8th Atmospheric and Space Environments Conference sponsored by the American Institute of Aeronautics and Astronautics, Washington D.C., June 13-17, 2016.""AIAA-2016-3733."Includes bibliographical references (pages 32-34).Aerodynamic characteristicsnasatAircraft icingnasatComputational fluid dynamicsnasatComputerized simulationnasatThree dimensional modelsnasatAerodynamic characteristics.Aircraft icing.Computational fluid dynamics.Computerized simulation.Three dimensional models.Broeren Andy P.1386216NASA Glenn Research Center,GPOGPOBOOK9910707944203321Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel3532254UNINA