LEADER 01661oam 2200481 a 450 001 9910702194303321 005 20120910155843.0 035 $a(CKB)5470000002424191 035 $a(OCoLC)809564942 035 $a(EXLCZ)995470000002424191 100 $a20120910d1986 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSubsonic flow investigations on a cranked wing designed for high maneuverability$b[electronic resource] /$fDhanvada M. Rao 210 1$aHampton, Va. :$cVigyan Research Associates, Inc. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1986] 215 $a1 online resource (42 pages) $cillustrations 225 1 $aNASA contractor report ;$v178046 300 $aTitle from title screen (viewed Sept. 10, 2012). 300 $a"February 1986." 320 $aIncludes bibliographical references (page 11). 606 $aLongitudinal control$2nasat 606 $aManeuverability$2nasat 606 $aSubsonic flow$2nasat 606 $aSwept wings$2nasat 606 $aVortices$2nasat 615 7$aLongitudinal control. 615 7$aManeuverability. 615 7$aSubsonic flow. 615 7$aSwept wings. 615 7$aVortices. 700 $aRao$b Dhanvada M$01422805 712 02$aVigyan Research Associates. 712 02$aLangley Research Center. 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910702194303321 996 $aSubsonic flow investigations on a cranked wing designed for high maneuverability$93548328 997 $aUNINA