01579nam 2200445I 450 991071177000332120190102092143.0(CKB)5470000002486370(OCoLC)1080576806(EXLCZ)99547000000248637020190102j201811 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierMid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /Witold J. F. Koning [and three others]Moffett Field, CA :National Aeronautics and Space Administration, Ames Research Center,November 2018.1 online resource (viii, 32 pages) color illustrationsNASA/TM ;2018-219788"November 2018."Includes bibliographical references (page 32).Angle of attacknasatDirectional stabilitynasatRotary wing aircraftnasatComputational fluid dynamicsnasatWind tunnel testsnasatAngle of attack.Directional stability.Rotary wing aircraft.Computational fluid dynamics.Wind tunnel tests.Koning Witold J. F.1407258Ames Research Center,GPOGPOBOOK9910711770003321Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept3537832UNINA