LEADER 01782nam  2200505   450 
001 9910702781403321
005 20141117150005.0
035   $a(CKB)5470000002430382
035   $a(OCoLC)895681556
035   $a(EXLCZ)995470000002430382
100   $a20141117j201305    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputations on wings with full-span oscillating control surfaces using Navier-Stokes equations /$fGuru P. Guruswamy
210  1$aMoffett Field, CA :$cNational Aeronautics and Space Administration, Ames Research Center,$dMay 2013.
215   $a1 online resource (10 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2013-216601
300   $aTitle from title screen (viewed Nov. 17, 2014).
300   $a"May 2013."
320   $aIncludes bibliographical references (pages 9-10).
606   $aAerospace vehicles$2nasat
606   $aAircraft configurations$2nasat
606   $aRotary wing aircraft$2nasat
606   $aWing span$2nasat
606   $aOscillations$2nasat
606   $aControl surfaces$2nasat
606   $aParallel processing (computers)$2nasat
615  7$aAerospace vehicles.
615  7$aAircraft configurations.
615  7$aRotary wing aircraft.
615  7$aWing span.
615  7$aOscillations.
615  7$aControl surfaces.
615  7$aParallel processing (computers)
700   $aGuruswamy$b Guru P.$01388031
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702781403321
996   $aComputations on wings with full-span oscillating control surfaces using Navier-Stokes equations$93438388
997   $aUNINA