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