01781nam 2200469I 450 991070624810332120171018095708.0(CKB)5470000002455957(OCoLC)1006643793(EXLCZ)99547000000245595720171018j201707 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierLow-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /Andy P. Broeren [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,July 2017.1 online resource (39 pages) color illustrationsNASA/TM ;2017-219533"July 2017.""Prepared for the 9th AIAA Atmospheric and Space Environments Conference sponsored by AIAA, Denver, Colorado, June 5-9, 2017.""AIAA-2017-4372."Includes bibliographical references (pages 38-39).Aerodynamic configurationsnasatAircraft icingnasatComputational fluid dynamicsnasatLeading edgesnasatSwept wingsnasatAerodynamic configurations.Aircraft icing.Computational fluid dynamics.Leading edges.Swept wings.Broeren Andy P.1386216NASA Glenn Research Center,GPOGPOBOOK9910706248103321Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects3514422UNINA