LEADER 01579nam  2200445I  450 
001 9910711770003321
005 20190102092143.0
035   $a(CKB)5470000002486370
035   $a(OCoLC)1080576806
035   $a(EXLCZ)995470000002486370
100   $a20190102j201811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /$fWitold J. F. Koning [and three others]
210  1$aMoffett Field, CA :$cNational Aeronautics and Space Administration, Ames Research Center,$dNovember 2018.
215   $a1 online resource (viii, 32 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2018-219788
300   $a"November 2018."
320   $aIncludes bibliographical references (page 32).
606   $aAngle of attack$2nasat
606   $aDirectional stability$2nasat
606   $aRotary wing aircraft$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAngle of attack.
615  7$aDirectional stability.
615  7$aRotary wing aircraft.
615  7$aComputational fluid dynamics.
615  7$aWind tunnel tests.
700   $aKoning$b Witold J. F.$01407258
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910711770003321
996   $aMid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept$93537832
997   $aUNINA